Open davids5 opened 3 years ago
Removing the Help on V2 Saves
Strings Left are - @dagar - I thould we have errno set to numbers only, did that change?
@/dev/console /dev/ttySx %s: Hard Fault: %s: IRQ: %d regs: %p %s: BASEPRI: %08x PRIMASK: %08x IPSR: %08x CONTROL: %08x %s: CFAULTS: %08x HFAULTS: %08x DFAULTS: %08x BFAULTADDR: %08x AFAULTS: %08x %s: PANIC!!! Hard fault: %08x armv7-m/arm_hardfault.c arm_hardfault Idle Task init irq/irq_unexpectedisr.c <noname> hpwork lpwork ERROR: nsh_consolemain() returned: %d cromfs /etc /dev/ram0 fopen ftell loop /etc/init.d/rcS nsh_getdirpath chdir nsh_setvar nsh_unsetvar unsetenv OLDPWD readline nsh_session Usage: %s [<script-path>|-c <command>] malloc %s=%s [Ksched_getparm pthread_create %s [%d:%d] /tmp %s/TMP%d.dat exec stat unlink %s=%s while until fseek then else nice nsh: %s: argument invalid nsh: %s: value out of range nsh: %s: missing required argument(s) nsh: %s: %s failed: %s nsh: %s: command not found nsh: %s: out of memory nsh: %s: not valid in this context nsh: %s: nesting too deep nsh: %s: Internal error nsh: %s: no matching %s nsh: %s: no such %s: %s nsh: %s: Interrupted by signal nsh: %s: syntax error nsh: %s: too many arguments NuttShell (NSH) NuttX-10.0.0 nsh> %s %s %s usage: NSH command forms: [nice [-d <niceness>>]] <cmd> [> <file>|>> <file>] [&] if <cmd> then [sequence of <cmd>] else fi while <cmd> do done until <cmd> Where <cmd> is one of: help Builtin Apps: <script-path> <expression> ] break <path> [<path> [<path> ...]] [<dir-path>|-|~|..] <source-path> <dest-path> [-s "MMM DD HH:MM:SS YYYY"] echo [-n] [<string|$name> [<string|$name>...]] <hex-address> exit [<name> [<value>]] false free [-v] [<cmd>] kill -<signal> <pid> [-lRs] <dir-path> mkdir <path> mkfatfs [-F <fatsize>] [-r <rootdirentries>] <block-driver> -t <fstype> [-o <options>] [<block-device>] <mount-point> <old-path> <new-path> <hex-address>[=<hex-value>] [<hex-byte-count>] <file-path> rmdir [{+|-}{e|x|xe|ex}] [<name> <value>] <sec> source <expression> "<command>" true umount unset <name> usleep <usec> ---------- :F:r: rename %s/%s/status asprintf %5s %3s %-8s %-7s %3s %-8s %-9s %-8s %s/%s/cmdline Calling %p POLICY EVENT SIGMASK COMMAND /proc task Flags: Priority: Scheduler: SigMask: State: Type: /proc/meminfo clock_gettime %lu.%04lu sec clock_settime gmtime_r strftime %a, %b %d %H:%M:%S %Y %p = 0x%08x -> 0x%08x waitpid :o:t: NUTTX FAT12 FAT16 FAT32 %s: %08x: %08x %08x %08x %08x %08x %08x %08x %08x %s: %s: PID=%d Stack Used=%lu of %lu %s: Assertion failed at file:%s line: %d task: %s %s: R0: %08x %08x %08x %08x %08x %08x %08x %08x %s: R8: %08x %08x %08x %08x %08x %08x %08x %08x %s: xPSR: %08x BASEPRI: %08x CONTROL: %08x %s: EXC_RETURN: %08x %s: sp: %08x %s: IRQ stack: %s: base: %08x %s: size: %08x %s: used: %08x %s: ERROR: Stack pointer is not within the interrupt stack %s: User stack: %s: ERROR: Stack pointer is not within the allocated stack up_stackdump up_taskdump up_registerdump up_dumpstate up_assert (null) vH'B [%Co O8M2 uUnknown error Success Operation not permitted No such file or directory No such process Interrupted system call I/O error No such device or address Arg list too long Exec format error Bad file number No child processes Try again Out of memory Permission denied Bad address Block device required Device or resource busy File exists Cross-device link No such device Not a directory Is a directory Invalid argument File table overflow Too many open files Not a typewriter Text file busy File too large No space left on device Illegal seek Read-only file system Too many links Broken pipe Math argument out of domain of func Math result not representable No message of desired type Identifier removed Channel number out of range Level 2 not synchronized Level 3 halted Level 3 reset Link number out of range Protocol driver not attached No CSI structure available Level 2 halted Resource deadlock would occur No record locks available Invalid exchange Invalid request descriptor Exchange full No anode Invalid request code Invalid slot File locking deadlock error Bad font file format Device not a stream No data available Timer expired Out of streams resources Machine is not on the network Package not installed Object is remote Link has been severed Advertise error Srmount error Communication error on send Protocol error Multihop attempted Inode is remote RFS specific error Not a data message Inappropriate file type or format Name not unique on network File descriptor in bad state Remote address changed Can not access a needed shared library Accessing a corrupted shared library .lib section in a.out corrupted Attempting to link in too many shared libraries Cannot exec a shared library directly Function not implemented No more files Directory not empty File name too long Too many symbolic links encountered Operation not supported on transport endpoint Protocol family not supported Connection reset by peer No buffer space available Address family not supported by protocol Protocol wrong type for socket Socket operation on non-socket Protocol not available Cannot send after transport endpoint shutdown Connection refused Address already in use Software caused connection abort Network is unreachable Network is down Connection timed out Host is down No route to host Operation now in progress Socket already connected Destination address required Message too long Protocol not supported Socket type not supported Cannot assign requested address Network dropped connection because of reset Transport endpoint is already connected Transport endpoint is not connected Too many references: cannot splice Limit would be exceeded by attempted fork Too many users Quota exceeded Stale NFS file handle Not supported No medium found No such host or network path Filename exists with different case Illegal byte sequence Value too large for defined data type Operation cancelled State not recoverable Previous owner died Streams pipe error %02d %03d %04d January February March April June July August September October November December Sunday Monday Tuesday Wednesday Thursday Friday Saturday OLDPWD /dev/ttyACM%d Bulk 3D Robotics PX4 FMU v2.x /dev/null /dev/ram%d /dev/tmpc%06lx binfs procfs vfat 0123456789ABCDEF -rom1fs- [0-9]*/** [0-9]* self self/** uptime version Name: %-12s%s Type: State: Flags: %-12s%c%c%c Priority: %-12s%d (%d) Scheduler: SigMask: %-12s%08x 0x%p StackBase: %-12s0x%p StackSize: %-12s%ld StackUsed: %-12s0x%02x Members: %-12s%d %-3s %-8s %s OFLAGS %3d %8ld %04x Task pthread Kthread Invalid Waiting,Unlock Ready Running Inactive Waiting,Semaphore Waiting,Signal Stopped group/fd group/status group stack SCHED_FIFO SCHED_RR SCHED_SPORADIC SCHED_OTHER %10.2f total used free largest Umem: %11lu%11lu%11lu%11lu %s version %s %s <pthread> nxtask_spawn_proxy ms5611 fw_att_control vmount mavlink rc_update tone_alarm commander airspeed_selector bl_update ekf2 navigator hardfault_log lsm303d sercon mpu6000 param fw_pos_control_l1 mc_att_control l3gd20 pwm_out battery_status land_detector hmc5883 serdis ms4525_airspeed mc_rate_control load_mon logger tune_control board_adc mc_pos_control uorb sensors mc_hover_thrust_estimator sercon:: ERROR: Already connected sercon: Registering CDC/ACM serial driver sercon: ERROR: Failed to create the CDC/ACM serial device: %d sercon: Successfully registered the CDC/ACM serial driver serdis: ERROR: Not connected serdis: Disconnected NuttX 10.0.0 bc0e6e37bf-dirty %s %s %s 04:37:03 Dec 17 2020 /dev/tmpb%06lx /dev/mtdblock%d already loaded uorb manager alloc failed uorb is not running Failed to allocate DeviceMaster %s advertise failed (%i) orb_advertise_multi: failed to set queue size px4_ioctl ORBIOCGADVERTISER failed. fd = %d orb_publish failed %s /%s/%s%d addNewDeviceNodes failed (%i) TOPIC NAME %-*s INST #SUB #Q SIZE PATH no active topics [Kupdate: 1s, num topics: %i [K%-*s INST #SUB RATE #Q SIZE [K%-*s %2i %4i %4i %2i %4i %-*s %2i %4i %2i %4i %s CDev::open failed board_adc: sample PX4_MAX_ADC_CHANNELS is too small (%d, %d) arch adc init failed sample timeout DeviceID: %d Resolution: %d Voltage Reference: %f % 2d:% 6d ADC test failed. ADC test successful. unknown command timeout, forcing stop usage Task already running Task start failed (%i) wq:hp_default ms5607 device: %s ms5611: read ms5611: measure ms5611: com_err %s measure error GPS_%i_PROTOCOL ERR: unknown baudrate: %d ERR: %d (cfsetispeed) ERR: %d (cfsetospeed) ERR: %d (tcsetattr) Reset is not supported on this device. Reset failed. Reset succeeded. NOT OK disabled Main GPS Secondary GPS protocol: SIMULATED protocol: UBX protocol: MTK protocol: ASHTECH protocol: EMLIDREACH status: %s, port: %s, baudrate: %d sat info: %s rate reading: %6i B/s rate position: %6.2f Hz rate velocity: %6.2f Hz rate publication: %6.2f Hz rate RTCM injection: %6.2f Hz /dev/ttyS3 b:d:e:fg:si:j:p: baudrate parsing failed uart unknown interface: %s unknown interface for secondary: %s unknown protocol: %s unrecognized flag Timed out while waiting for thread to start cold warm Resetting GPS - %s GPS_DUMP_COMM failed to allocated dump data GPS: failed to open serial port: %s err: %d GPS_YAW_OFFSET GPS_UBX_DYNMODEL GPS_UBX_MODE failed to instantiate object MTK: Unsupported Output Mode %i $PMTK220,200*2C mtk: config write failed $PGCMD,16,0,0,0,0,0*6A $PMTK313,1*2E $PMTK301,2*2E $PMTK397,0*23 mtk: unknown revision $PASHS,NME,POS,%c,ON,0.2 $PASHS,RT3,1074,%c,ON,1 $PASHS,RT3,1084,%c,ON,1 $PASHS,RT3,1094,%c,ON,1 $PASHS,RT3,1114,%c,ON,1 $PASHS,RT3,1124,%c,ON,1 $PASHS,RT3,1006,%c,ON,1 $PASHS,RT3,1033,%c,ON,31 $PASHS,RT3,1013,%c,ON,1 $PASHS,RT3,1029,%c,ON,1 $PASHS,RT3,1230,%c,ON $PASHS,RT3,1005,%c,ON,1 $PASHS,RT3,1077,%c,ON,1 $PASHS,RT3,1087,%c,ON,1 $PASHS,NME,ALL,%c,OFF $PASHS,ATM,ALL,%c,OFF $PASHS,OUT,%c,ON $PASHS,NME,ZDA,%c,ON,3 $PASHS,NME,GST,%c,ON,3 $PASHS,NME,POS,%c,ON,0.05 $PASHS,NME,GSV,%c,ON,1 $PASHS,ANP,OWN,TRM55971.00 $PASHS,STI,0001 $PASHQ,PRT $PASHS,SPD,%c,9 $PASHS,SNS,DUO,2 $PASHQ,RID $PASHS,POP,20 $PASHS,SNS,SOL $PASHS,NME,HDT,%c,ON,0.05 $PASHS,POS,%.8f,%c,%.8f,%c,%.5f,PC1 $PASHS,POS,AVG,%i ZDA, GGA, $GPHDT, $PASHR,POS, GST, GSV, $PASHR,NAK $PASHR,ACK $PASHR,PRT, $PASHR,RID, $PASHR,RECEIPT, FINISHED, FIXME: use of deprecated msg CFG_MSG (%i %i) 00040005 00040007 00070000 00080000 00190000 unknown board hw: %s MOD= buf for CFG_VALSET too small ubx msg 0x%04x invalid len %u ubx internal err1 TMODE3 failed. Device w/o base station support? ubx msg: %s ubx poll_or_read err EMLIDREACH: Unsupported Output Mode %i regdump testerror gyro reads: %u checked_next: %u reg %02x:%02x should be %02x l3gd20: read l3gd20: err l3gd20: bad_reg l3gd20: dupe %s FAILED TO DISABLE I2C L3GD20 registers %02x:%02x !"#$.9 lsm303d: acc_read lsm303d: mag_read lsm303d: bad_reg lsm303d: bad_val lsm303d: acc_dupe %s SPI init failed (%i) !"#$%& FIFO empty interval: %d us (%.1f Hz) mpu6000: bad register mpu6000: bad transfer mpu6000: FIFO empty mpu6000: FIFO overflow mpu6000: FIFO reset mpu6000: DRDY missed %s unexpected WHO_AM_I 0x%02x %s SPI::init failed (%i) interval: %u us hmc5883: read hmc5883: com_err hmc5883: rng_err hmc5883: conf_err %s read_reg fail %s ID byte mismatch (%02x,%02x,%02x) %s SPI init failed cap6 no pwm pwm8 cap4 cap5 Max update rate: %i Hz PWM Mode: %s /dev/px4fmu pwm_out: cycle pwm_out: interval rate group %u mask %x bad overlap %x rate group set alt failed rate group set default failed PWM_MAIN_REV%d PWM_AUX_REV%d PWM REV only for MAIN and AUX PWM_MAIN_TRIM%d PWM_AUX_TRIM%d PWM TRIM only for MAIN and AUX FMU: Capture chan:%d time:%lld state:%d overflow:%d error: no mixer loaded warning: trim values not valid - no mixer loaded open fail Failed to Enter pwm test mode servo arm failed Unable to get servo count Not in a capture mode Testing %u servos and %u input captures Unable to get capture callback for chan %u Unable to set capture callback for chan %u Press CTRL-C or 'c' to abort. servo %u set failed error reading PWM servo %d servo %d readback error, got %u expected %u Unable to get stats for chan %u FMU: Status chan:%u edges: %d last time:%lld last state:%d overflows:%d lantency:%u User abort Failed to Exit pwm test mode setting I2C clock failed not enough arguments sensor_reset reset default time peripheral_reset mode_gpio mode_pwm mode_pwm1 mode_pwm6 mode_pwm5 mode_pwm5cap1 mode_pwm4 mode_pwm4cap1 mode_pwm4cap2 mode_pwm3 mode_pwm3cap1 mode_pwm2 mode_pwm2cap2 /dev/pwm_output FAILED registering class device /etc/extras/px4_io-v2_default.bin /fs/microsd/px4_io-v2_default.bin /fs/microsd/px4io2.bin cannot alloc interface interface init failed /dev/px4io io update io write io control latency [IO] binding DSM%s RX binding failed. [IO] safety off, bind request rejected RC_MAP_ROLL RC_MAP_PITCH RC_MAP_YAW RC_MAP_THROTTLE RC_MAP_FLAPS RC_MAP_AUX1 RC_MAP_AUX2 RC_MAP_AUX3 RC_MAP_MODE_SW RC%u_MIN RC%u_TRIM RC%u_MAX RC%u_DZ RC%u_REV rc config upload failed config for RC%u rejected by IO actuator subscription failed CBRK_FLIGHTTERM poll error %d RC_FAILS_THR failsafe upload failed, FS: %d us CBRK_IO_SAFETY RC_RSSI_PWM_CHAN RC_RSSI_PWM_MAX RC_RSSI_PWM_MIN SENS_EN_THERMAL PWM_MAIN_REV%u PWM_MAIN_TRIM%u TRIM_ROLL TRIM_PITCH TRIM_YAW FW_MAN_R_SC FW_MAN_P_SC FW_MAN_Y_SC PWM_SBUS_MODE THR_MDL_FAC MOT_SLEW_MAX MC_AIRMODE /dev/pwm_output0 /dev/ttyS0 IO CONSOLE: %s fmu sent: "%s" mixer send error %d [IO] mixer upload fail DSM10 DSM11 FRAME_DROP FAILSAFE MAPPING_OK S.BUS1_OUT S.BUS2_OUT RSSI_PWM RSSI_ADC ENABLED REVERSED protocol %u hardware %u bootloader %u buffer %uB crc 0x%04x%04x %u controls %u actuators %u R/C inputs %u analog inputs %u relays reversed outputs: [ trims: r: %8.4f p: %8.4f y: %8.4f %hu raw R/C inputs R/C flags: 0x%04hx%s%s%s%s%s RC data (PPM frame len) %d us WARNING WARNING WARNING! This RC receiver does not allow safe frame detection. mapped R/C inputs 0x%04hx %u:%hd ADC inputs features 0x%04hx%s%s%s%s rates 0x%04x default %u alt %u sbus %u debuglevel %u controls %u: %hd input %u min %u center %u max %u deadzone %u assigned %u options 0x%04hx%s%s disarmed values IMU heater off IMU heater level %d HITL Mode PX4IO Not Supported driver allocation failed norc unknown argument: %s driver init failed detect checkcrc usage: px4io checkcrc filename open of %s failed: %d check CRC failed: %d loaded, detaching first PX4IO firmware file not found error updating PX4IO - check that bootloader mode is enabled verify failed - retry the update timed out waiting for bootloader - power-cycle and try again unexpected error %d forceupdate usage: px4io forceupdate MAGIC filename px4io is not started, still attempting upgrade reboot failed - %d safety_off failed to disable safety safety_on failed to enable safety recovery debug usage: px4io debug LEVEL SET_DEBUG failed: %d SET_DEBUG %hhu OK rx_dsm rx_dsm_10bit rx_dsm_11bit rx_sbus rx_ppm receiver type is automatically detected, option '%s' is deprecated poll fail [ Use 'px4io debug <N>' for more output. Hit <enter> three times to exit monitor mode ] driver not loaded, exiting bind needs argument, use dsm2, dsmx or dsmx8 dsm2 dsmx unknown parameter %s, use dsm2, dsmx or dsmx8 system must not be armed disable WARNING: ACTUATORS WILL BE LIVE IN HIL! PROCEED? Press 'y' to enable, any other key to abort. TIMEOUT! ABORTED WITHOUT CHANGES. WARNING: ACTUATORS ARE NOW LIVE IN HIL! ACTUATORS ARE NOW SAFE IN HIL. sbus1_out S.BUS v1 failed sbus2_out S.BUS v2 failed rssi_analog RSSI analog failed rssi_pwm RSSI PWM failed test_fmu_fail test_fmu_ok need a command, try 'start', 'stop', 'status', 'monitor', 'debug <level>', 'recovery', 'bind', 'checkcrc', 'safety_on', 'safety_off', 'forceupdate', 'update', 'sbus1_out', 'sbus2_out', 'rssi_analog' or 'rssi_pwm', 'test_fmu_fail', 'test_fmu_ok' IO not installed IO version error IO VERSION MISMATCH, PLEASE UPGRADE SOFTWARE! IO found SYS_RESTART_TYPE IO protocol/firmware mismatch, abort. config read error [IO] config read fail, abort. RECOVERING FROM FMU IN-AIR RESTART Failed to recover from in-air restart (1), abort MAV_SYS_ID MAV_COMP_ID PRM SYSID PRM CMPID IO is in failsafe, force failsafe Failed to recover from in-air restart (3), abort re-sending flight termination cmd Failed to recover from in-air restart (2), abort re-sending arm cmd failed disabling RC handling IO RC config upload fail default PWM output device task start failed: %d Failed to communicate with IO, abort. PX4IO_serial io_txns 8?61$#*-pw~ylkbeHOFATSZ] ' ).;<52 WPY^KLEBohafst}z ing`ur{|QV_XMJCD !&/(=:34NI@GRU\[vqx jmdc>907"%,+ read of %u bytes needed %u retries [PX4IO] bad sync 0x%02x,0x%02x erase... Can't allocate program buffer ../../src/drivers/px4io/px4io_uploader.cpp programming %u bytes... firmware read of %u bytes at %u failed -> %d errno %d verify... %d: got %d waiting for bytes %d: got 0x%02x expected 0x%02x timeout waiting for post-verify sync could not read firmware size did not receive CRC checksum CRC wrong: received: %d, expected: %d no firmware found failed to open %s using firmware from %s /dev/ttyS4 could not open interface Failed to stat %s - %d found bootloader revision: %d found unsupported bootloader revision %d, exiting erase failed program failed verify failed reboot failed bootloader not responding tune_control callback registration failed! CBRK_BUZZER Invalid tune: %d No airspeed sensor detected. Switch to non-airspeed mode. Primary airspeed index bigger than number connected sensors. Take last sensor. Airspeed: can't estimate scale as no valid sensor. Airspeed: estimated scale (ASPD_ASPD_SCALE): %0.2f airspeed_selector: elapsed Airspeed: switched from sensor %i to %i wq:nav_and_controllers BAT_V_OFFS_CURR BAT%d_V_DIV BAT%d_A_PER_V BAT%d_V_CHANNEL BAT%d_I_CHANNEL BAT_V_DIV BAT_A_PER_V BAT_ADC_CHANNEL arming: %s Armed Disarmed %s by %s REJECT %s Mission #%d loaded, %u WPs, curr: %d reading mission state failed Data link regained Onboard controller regained Connection to ground station lost Connection to mission computer lost High latency data link lost OFFBOARD AUTO RTL AUTO HOLD m slot overflow AUTO MISSION AUTO LAND AUTO TAKEOFF AUTO FOLLOW POSITION CONTROL ALTITUDE CONTROL STABILIZED ESC%d %soffline Reposition command rejected Unsupported auto mode Unsupported ARM_DISARM param: %.3f Arming denied! Already armed Arming denied! Not landed Disarming denied! Not landed Arming denied! Preflight checks have failed Arming denied! Throttle not centered Arming denied! Throttle not zero forcing lockdown (motors off) forcing failsafe (termination) reset all non-flighttermination failsafe commands disabling failsafe and lockdown Returning to launch Return to launch denied Takeoff denied! Please disarm and retry Landing at current position Landing denied! Please land manually Precision landing Precision landing denied! Please land manually Mission start denied Mission start denied! No valid mission Control high latency failed! Telemetry unavailable Calibration: Disabling RC input Calibration: Restoring RC input Stopping compass use! Check calibration on landing Critical navigation failure! Check sensor calibration RC_MAP_ARM_SW CASA Outback Challenge rules (NAV_DLL_ACT = 4) retired CASA Outback Challenge rules (NAV_RCL_ACT = 4) retired Yaw Airmode requires the use of an Arm Switch USB disconnected, rebooting for flight safety Landing detected Takeoff detected Mission cannot be completed Flight termination because of geofence Geofence violation! Flight terminated Pilot took over control using sticks Flight termination active Manual control regained after %.1fs Not arming: Switch to a manual mode first Not arming: Geofence RTL requires valid home Not arming: Preflight checks failed Landed, unable to retract landing gear Kill-switch disengaged Manual control lost Engine Failure vehicle_command lost, generation %d -> %d ESCs did not respond to arm request Critical failure detected: lockdown Critical failure detected: terminate flight Failsafe mode activated Failsafe mode deactivated Kill-switch engaged RC (switch) internal command external command mission start safety button auto preflight disarming kill-switch failure detector shutdown request unit tests /dev/led0 LED: open %s failed (%i) Amber LED: ioctl fail battery unavailable [cal] calibration failed: %s Disconnect battery and try again [cal] calibration started: 2 %s Can't open PWM device Unable to disable safety switch Unable to arm system Unable to force safety off [cal] Connect battery now Timeout waiting for battery [cal] Battery connected Safety switch still off Servos still armed Safety switch still deactivated [cal] calibration done: %s Transition denied: %s to %s Failsafe enabled: %s Low battery level! Return advised %s, landing advised %s, executing RTL %s, can't execute RTL, landing instead %s, landing %s, please land! Battery failure detected STANDBY STANDBY_ERROR SHUTDOWN IN_AIR_RESTORE No manual control stick input no datalink no offboard no local position no global position no RC and no offboard Critical battery level! Dangerous battery level! join failed: %d Failed to start thread (%i) commander_low_prio Error loading settings Error saving settings pthread_mutexattr_init failed, status=%d pthread_mutexattr_settype failed, status=%d pthread_mutex_init failed, status=%d [cal] calibration failed: reading sensor ERROR: cannot open calibration storage calibration save failed [cal] Hold still, measuring %s side [cal] accel %d invalid X-axis, check rotation [cal] accel %d invalid Y-axis, check rotation [cal] accel %d invalid Z-axis, check rotation [cal] %s side result: [%.3f %.3f %.3f] [cal] progress <%u> accel /dev/airspeed0 SENS_DPRES_ANSC [cal] airspeed offset zero failed [cal] No airspeed sensor found SENS_DPRES_OFF [cal] calibration failed: to set parameters [cal] Ensure sensor is not measuring wind [cal] Airspeed sensor is reporting errors (%llu) [cal] Check wiring, reboot vehicle, and try again [cal] airspeed offset update failed [cal] Offset of %d Pascal [cal] Blow across front of pitot without touching [cal] Positive pressure: OK (%d Pa) [cal] Negative pressure difference detected (%d Pa) [cal] Swap static and dynamic ports! [cal] Create air pressure! (got %d, wanted: 50 Pa) [cal] detected rest position, hold still... [cal] detected motion, hold still... ERROR: invalid orientation [cal] calibration cancelled command denied during calibration: %u timeout: no motion [cal] pending:%s [cal] hold vehicle still on a pending side [cal] %s side already completed [cal] %s orientation detected [cal] %s side done, rotate to a different side back front left right CAL_ SYS_FAC_CAL_MODE param export failed (%i) /fs/mtd_caldata Storing parameters to factory storage %s Detected %u gyros, but will calibrate only %u No gyros found ERROR: missing data, sensor %d motion, retrying.. ERROR: Motion during calibration gyro level SENS_BOARD_X_OFF SENS_BOARD_Y_OFF SENS_BOARD_ROT attitude estimator not running - check system boot motion during calibration excess roll angle excess pitch angle Updating SENS_BOARD_X_OFF %.1f -> %.1f degrees Updating SENS_BOARD_Y_OFF %.1f -> %.1f degrees External ERROR: out of memory Mag: %d sphere fitness: %.5f radius: %.4f Mag: %d ellipsoid fitness: %.5f Retry calibration (unable to fit mag %u) Retry calibration (sphere NaN, %u) Retry calibration (mag %u sphere radius invaid %.3f) Retry calibration (mag %u with non-positive scale) Warning: mag %u with large offsets [cal] External Mag: %d (%d), keeping manually configured rotation %d [cal] External Mag: %d (%d), determined rotation: %d [cal] External Mag: %d (%d), no rotation change: %d External Mag: %d (%d), determining rotation failed [cal] Internal Mag: %d (%d) rotation %d relative to primary %d (%d) %s Mag: %d (%d), rotation: %d, MSE: %.3f EKF2_MAGBIAS_%c CAL_MAG_ROT_AUTO CAL_MAG_SIDES [cal] Rotate vehicle gyro int: %8.4f, %8.4f, %8.4f Failed: This calibration requires rotation. [cal] %s side calibration: progress <%u> GPS required for mag quick cal attitude required for mag quick cal Assuming vehicle is facing heading %.1f degrees Mag quick calibration finished no inputs, aborting TRIM: PARAM SET FAIL trim cal done Could not open data manager file %s Could not seek data manager file %s Failed writing compat: %d Could not allocate %d bytes of memory In flight restart Power on restart Unknown restart No valid backend set. dataman: read dataman: write %s, data manager file '%s' size is %d bytes %s, data manager RAM size is %d bytes dataman already running f:ri dataman file set to: %s -f, -r and -i are mutually exclusive RAM/Flash backend is not available /fs/microsd/dataman task start failed dataman start failed dataman worker thread not running Writes %d Reads %d Clears %d Restarts %d Max Q lengths work %d, free %d poweronrestart inflightrestart ekf2:%d attitude: %d, local position: %d, global position: %d ekf2: ECL update ekf2: ECL full update replay mode enabled module locked, try again later stopping instance %d invalid instance %d stopping ekf2 instance %d %d - found range finder with instance %d %d - mag sensor ID changed to %i %d - resetting IMU bias %d - failed to register callback, retrying wq:INS0 vehicle attitude callback registration failed! fw_att_control: cycle VT_TYPE vtol yaw rate sepoint not finite vehicle local position callback registration failed! Airspeed parameters invalid Landing aborted fw_pos_control_l1: cycle VT_ARSP_TRANS Landing, heading hold Landing, limiting throttle Landing, flaring Landing, on slope Takeoff on runway Launch detection running fixedwing multicopter rover airship unknown mode running (%s) land_detector: cycle LNDMC_Z_VEL_MAX > MPC_LAND_SPEED, updating %.3f -> %.3f MPC_LAND_SPEED MPC_MANTHR_MIN MPC_THR_MIN MPC_USE_HTE MPC_THR_HOVER load_mon: cycle %s low on stack! (%i bytes left) %s low on FDs! (%i FDs left) wq:lp_default logger not running Log file: %s/%s/%s Wrote %4.2f KiB (avg %5.2f KiB/s) Wrote %4.2f MiB (avg %5.2f KiB/s) Since last status: dropouts: %zu (max len: %.3f s), max used buffer: %zu / %zu B Failed to find topic %s r:b:etfm:p:x unknown mode: %s several Running in mode: %s Number of subscriptions: %i (%i bytes) Full File Logging Running: Mission File Logging Running: Mavlink Logging Running (Full log) Not logging No logging profile selected. Using default set Max num mission topics exceeded (%i) /fs/microsd/mission_log failed creating log root dir: %s (%i) Logging FIFO data: increasing task prio and logging rate pthread_setschedparam failed (%i) battery_status not published. Logging anyway log path too long %Y-%m-%d failed creating new dir: %s failed creating new dir: %s (%i) _replayed %s%s.ulg log%03u%s.ulg Stop mavlink log Writing watchdog data max recursion level reached (%i) %s:%s Array too small invalid format %s buf len too small uint8_t uint16_t uint32_t uint64_t float double bool char No definition for topic %s found limit for _next_topic_id reached No subscriptions added char[%zu] %s info_multiple str too long (%i), key=%s perf_counter_preflight perf_counter_postflight perf_top ver_sw ver_sw_release ver_vendor_sw_release PX4_FMU_V2 ver_hw ver_hw_subtype sys_name sys_os_name ver_sw_branch sys_os_ver sys_os_ver_release sys_toolchain sys_toolchain_ver sys_lib_ecl_ver %s, rev. %c sys_mcu ver_data_format sys_uuid time_ref_utc replay log_type Start file log (type: %s) failed to get log file name [logger] %s Start mavlink log logger started (mode=%s) /fs/microsd/log log root dir created: %s failed to alloc message buffer writer init failed Failed to subscribe (%i) poll failed (%i) perf_top_preflight perf_top_postflight perf_top_watchdog LogWriterFile allocation failed LogWriterMavlink allocation failed failed to create writer thread (%i) mavlink init failed logger_sd_write logger_sd_fsync logger_sd_write_mission logger_sd_fsync_mission /fs/bbr3 ULog file name too long (%s, %i>=%i) unknown Can't open log file %s, errno: %d Can't create log buffer Failed to register ULog file to the hardfault handler (%i) Opened %s log file: %s closing log file failed (%i) closed logfile, bytes written: %zu write failed (%i) log_writer_file Ack timeout. Stopping mavlink log sess%d %d-%d-%d %s/sess%03u %s/%04u-%02u-%02u log path too long (%i) removing log directory %s to get more space (left=%u MiB) Failed to delete directory [logger] Not logging; SD almost full: %u MiB watchdog init failed skip topic %s, format string is too large: %zu (max is %zu) Too many subscriptions, failed to add: %s %d actuator_controls_0 actuator_outputs manual_control_setpoint rate_ctrl_status sensor_combined vehicle_angular_acceleration vehicle_angular_velocity vehicle_attitude vehicle_attitude_setpoint vehicle_rates_setpoint collision_constraints obstacle_distance_fused vehicle_mocap_odometry vehicle_trajectory_waypoint vehicle_trajectory_waypoint_desired vehicle_visual_odometry sensor_gyro_fifo sensor_accel_fifo actuator_controls_1 camera_capture mission_result vehicle_global_position actuator_armed airspeed_validated camera_trigger camera_trigger_secondary cellular_status commander_state cpuload esc_status generator_status home_position hover_thrust_estimate input_rc manual_control_switches navigator_mission_item offboard_control_mode onboard_computer_status position_controller_status position_setpoint_triplet px4io_status radio_status sensor_correction sensor_gyro_fft sensor_preflight_mag sensor_selection sensors_status_imu system_power tecs_status test_motor trajectory_setpoint transponder_report vehicle_acceleration vehicle_air_data vehicle_command vehicle_constraints vehicle_control_mode vehicle_gps_position vehicle_land_detected vehicle_local_position vehicle_local_position_setpoint vehicle_magnetometer vehicle_roi vehicle_status_flags vtol_vehicle_status logger_status multirotor_motor_limits telemetry_status estimator_selector_status ekf_gps_drift estimator_attitude estimator_global_position estimator_innovation_test_ratios estimator_innovation_variances estimator_innovations estimator_optical_flow_vel estimator_local_position estimator_sensor_bias estimator_states estimator_visual_odometry_aligned yaw_estimator_status wind_estimate differential_pressure distance_sensor optical_flow sensor_accel sensor_baro sensor_gps sensor_gyro sensor_mag vehicle_imu vehicle_imu_status gps_dump debug_array debug_key_value debug_value debug_vect satellite_info ekf2_timestamps %s %u %u Failed to add topic %s /fs/microsd/etc/logging/logger_topics.txt logging %d topics from logger_topics.txt ALTITUDE ATTITUDE ATTITUDE_QUATERNION ATTITUDE_TARGET AUTOPILOT_VERSION COLLISION DISTANCE_SENSOR ESC_INFO ESC_STATUS EXTENDED_SYS_STATE FLIGHT_INFORMATION GPS_GLOBAL_ORIGIN GPS_STATUS HIGH_LATENCY2 HIL_STATE_QUATERNION MOUNT_ORIENTATION OBSTACLE_DISTANCE OPTICAL_FLOW_RAD ORBIT_EXECUTION_STATUS PROTOCOL_VERSION RAW_RPM STATUSTEXT STORAGE_INFORMATION WIND_COV HEARTBEAT COMMAND_LONG SYS_STATUS BATTERY_STATUS SMART_BATTERY_INFO HIGHRES_IMU SCALED_IMU SCALED_IMU2 SCALED_IMU3 VFR_HUD GPS_RAW_INT GPS2_RAW SYSTEM_TIME TIMESYNC ADSB_VEHICLE UTM_GLOBAL_POSITION CAMERA_TRIGGER CAMERA_IMAGE_CAPTURED GLOBAL_POSITION_INT ODOMETRY LOCAL_POSITION_NED ESTIMATOR_STATUS VIBRATION ATT_POS_MOCAP HOME_POSITION HIL_ACTUATOR_CONTROLS POSITION_TARGET_GLOBAL_INT POSITION_TARGET_LOCAL_NED RC_CHANNELS MANUAL_CONTROL TRAJECTORY_REPRESENTATION_WAYPOINTS NAV_CONTROLLER_OUTPUT CAMERA_CAPTURE ACTUATOR_CONTROL_TARGET1 ACTUATOR_CONTROL_TARGET0 SERVO_OUTPUT_RAW_1 SERVO_OUTPUT_RAW_0 SCALED_PRESSURE File open failed %s readdir failed %s %d FTP: Open failed - out of sessions request past EOF seek fail read fail %d write fail %d cp: read cp: short write /fs/microsd/.trunc.tmp /fs/microsd/logdata.txt %u %u %s /fs/microsd/$log$.txt sess .px4log %u %u %s instance ID is out of range MAV_TYPE parameter invalid, resetting to 0. /dev/ttyS1 mavlink: tx run elapsed mavlink: tx run interval mavlink: send_bytes error mavlink: send_start tx buffer full waiting for instances to stop Couldn't stop all mavlink instances. all instances stopped /fs/microsd channel %d has missed %d mavlink log messages Session was closed without activity Failed to allocate buffers ATS3=%u AT&F AT&W open fd %d failed Unknown GCS heartbeat valid mavlink chan: #%u type: RADIO Link rssi: %d remote rssi: %u txbuf: %u noise: %d remote noise: %u rx errors: %u fixed: %u USB CDC GENERIC LINK OR RADIO no radio status. flow control: %s rates: tx: %.3f kB/s txerr: %.3f kB/s tx rate mult: %.3f tx rate max: %i B/s rx: %.3f kB/s ULog rate: %.1f%% of max %.1f%% FTP enabled: %s, TX enabled: %s mode: %s MAVLink version: %i transport protocol: serial (%s @%i) ping statistics: last: %0.2f ms mean: %0.2f ms max: %0.2f ms min: %0.2f ms dropped packets: %u mavlink for device %s is not running DM_KEY_MISSION_STATE lock failed offboard mission init failed (%i) WPM: can't save mission state Mission storage: Unable to write to microSD ERROR: wp index out of bounds WPM: MAX_COUNT out of bounds (%u) WPM: _count out of bounds (%u) ERROR: Waypoint index exceeds list capacity WPM: WP CURR CMD: Error setting ID WPM: MISSION_SET_CURRENT seq=%d ERROR: not in list WPM: WP CURR CMD: Not in list WPM: IGN WP CURR CMD: Busy mission type %u not handled locking failed (%i) WPM: REJ. CMD: Busy WPM: IGN MISSION_COUNT: Busy Mission ack result was %d REJ. WP CMD: partner id mismatch Mission download request ignored, already active WPM: IGN CLEAR CMD: Busy Received unknown mission type, abort. Mission storage: Unable to read from microSD WPM: Unexpected mission type (%u %u) WPM: REJ. CMD: Req. WP was unexpected WPM: REJ. CMD: partner id mismatch _HASH_CHECK Operation timeout [mavlink: component %d] %.50s Stopping mavlink shell Starting mavlink shell mavlink_shell Failed to allocate a shell Failed to start shell (%i) SimpleAnalyzer: Unknown mode. COM_FLIGHT_UUID [timesync] Time jump detected. Resetting time synchroniser. [timesync] RTT too high for timesync: %llu ms (sender: %i) [timesync] Failed setting realtime clock no ack from logger (is it running?) Maximum MAVLink instance count of %d reached. mavlink_if%d Tune string too long. Could not allocate tune publisher Tune format %d not supported cmd sender %s handling result %d for command %d (from %d:%d) %s new command: %d (channel: %d) %s command %d sent (not first, retries: %d/%d, channel: %d) %s command %d dropped %s command %d sent (first, retries: %d/%d, channel: %d) instance %d: RADIO_STATUS timeout Message Size (if active) [B] Rate Config (current) [Hz] Name %-20s%-16s %s unlimited %6.2f (%.3f) %-30s%-16s %3i instance #%u: mavlink stop is deprecated, use stop-all instead stop-all streams boot_complete stream %s not found NAMED_VALUE_FLOAT setting stream %s to default failed stream %s on device %s not found Unsupported baudrate: %d supported examples: 9600, 19200, 38400, 57600 115200 230400 460800 500000 921600 1000000 ERR GET CONF %s: %d ERR SET BAUD %s: %d ERR SET CONF %s hardware flow control not supported Got unsuccessful result %d from camera b:r:d:n:u:o:m:t:c:fswxzZ invalid baud rate '%s' datarate parsing failed invalid data rate '%s' Device %s does not exist UDP options not supported on this platform invalid mode custom onboard magic config iridium minimal extvision extvisionmin /dev/ttyACM0 /dev/ttyACM1 %s already running mode: %s, data rate: %d B/s on %s @ %dB msg buf alloc fail configure_streams_to_default() failed could not open %s Disable transmitting with IRIDIUM mavlink on device %s Enable transmitting with IRIDIUM mavlink on device %s Enable transmitting with IRIDIUM mavlink on device %s by command Disable transmitting with IRIDIUM mavlink on device %s by command mavlink ulog stream update failed, stopping (%i) exiting channel %i OUT OF MEM IGN MISSION_ITEM: No transfer IGN MISSION_ITEM: Busy Fence: too few vertices Unable to write on micro SD [pm] unknown param: %s [pm] param types mismatch param: %s [pm] unknown param ID: %u [pm] failed loading param from storage ID: %u parameter_rc_channel_index out of bounds force setpoint not supported ignoring CMD with same SYS/COMP (%d/%d) ID Not enough bandwidth to enable log streaming PX4Accelerometer alloc failed PX4Gyroscope alloc failed Body frame %u not supported. Unable to publish velocity Estimator source %u not supported. Unable to publish pose and velocity Local frame %u not supported. Unable to publish pose and velocity mavlink_rcv_if%d system boot did not complete in 20 seconds Normal Custom Onboard Magic Config Iridium Minimal ExtVision ExtVisionMin vRQ> 8STs LwH' vehicle_attitude callback registration failed! mc_att_control: cycle vehicle_local_position_setpoint callback registration failed! mc_hover_thrust_estimator: cycle time Running, active flight task: %i Running, no flight task active vehicle_local_position callback registration failed! Failsafe: stop and wait Failsafe: blind land Failsafe: blind descend Previous flight task failed, switching to mode %d Transition activation failed with error: %s Offboard activation failed with error: %s Follow-Me activation failed with error: %s Auto activation failed with error: %s Descend activation failed with error: %s Position-Ctrl activation failed with error: %s Altitude-Ctrl activation failed with error: %s Tilt constrained to safe value Land tilt has been constrained by max tilt Cruise speed has been constrained by max speed Manual speed has been constrained by max speed Hover thrust has been constrained by min/max VELD mc_pos_control: cycle time invalid setpoints vehicle_angular_velocity callback registration failed! mc_rate_control: cycle wq:rate_ctrl VT_B_DEC_MSS VT_B_REV_DEL Warning TRAFFIC %s! dst %d, hdg %d TRAFFIC: %s Returning home! dst %d, hdg %d TRAFFIC: %s Landing! dst %d, hdg % d TRAFFIC: %s Holding position! dst %d, hdg %d /fs/microsd/etc/geofence.txt Loading geofence from %s poll error %d, %d Reposition is outside geofence planned mission landing not available CMD_MISSION_START failed Geofence violation RTL LAND activated RTL Closest landing point activated RTL Mission activated, continue mission RTL Mission activated, fly mission in reverse RTL Mission activated, fly to home RTL HOME activated fencefile fake_traffic LX007 LX55 LX20 dataman read failure Can't save mission state Invalid mission state. Mission item index out of bound, index: %d, max: %d. Waypoint could not be read. DO JUMP waypoint could not be written. DO JUMP repetitions completed. DO JUMP is cycling, giving up. mission update failed mission check failed could not read mission item during reset could not save mission item during reset Could not read mission. Executing Reverse Mission Executing Mission Reverse Mission finished, landed Mission finished, landed. Reverse Mission finished, loitering Mission finished, loitering. No valid mission available, refusing takeoff. No valid mission available, loitering. Takeoff to %.1f meters above home. MissionReverse: Got a non-position mission item, ignoring it Holding at %d m above landing. dm_read failed RTL: unsupported MAV_FRAME RTL: using mission landing RTL: unable to use mission landing RTL: climb to %d m (%d m above destination) RTL: return at %d m (%d m above destination) RTL: descend to %d m (%d m above destination) RTL: completed, loitering RTL: loiter %.1fs RTL: land at destination RTL: landing at home position. RTL: landing at mission landing. RTL: landing at safe landing point. Using minimum takeoff altitude: %.2f m Already higher than takeoff altitude MPC_ACC_HOR MPC_XY_CRUISE Climbing to search altitude. Falling back to normal land. Can't switch to search or fallback landing Search timed out Can't switch to fallback landing Lost landing target while landing (descending). Resetting landing position to current position Lost landing target while landing (horizontal approach). Precision landing took too long during horizontal approach phase. Geofence requires valid home position Geofence violation for waypoint %zu Mission rejected: No home pos, WP %zu uses rel alt Warning: No home pos, WP %zu uses rel alt Mission rejected: Waypoint %zu below home Warning: Waypoint %zu below home Mission rejected: Cannot access SD card Mission rejected: item %i: unsupported cmd: %d Actuator number %d is out of bounds 0..5 Actuator value %d is out of bounds -PWM_DEFAULT_MAX..PWM_DEFAULT_MAX Mission rejected: starts with landing Mission rejected: Takeoff altitude too low! Mission rejected: takeoff waypoint required. Mission rejected: takeoff not first waypoint item Mission rejected: more than one land start. Mission rejected: waypoint within landing flare. Mission rejected: adjust landing approach. Move down %d m or move further away by %d m. Mission rejected: landing above last waypoint. Mission rejected: need landing approach. Mission rejected: starts with land waypoint. Mission rejected: land start item before RTL item not possible. Mission rejected: landing pattern required. Mission rejected: invalid land start. Error reading offboard mission. First waypoint too far away: %d meters, %d max. Distance between waypoints too far: %d meters, %d max. Distance between waypoint and gate too close: %d meters Not yet ready for mission, no position lock. Polygon with 0 vertices. Skipping unhandled Fence command: %i Frame type %i not supported DMS %lf %lf %lf %lf %lf %lf Scanf to parse DMS geofence vertex failed. Scanf to parse geofence vertex failed. Geofence: point: %d, lat %.5lf: lon: %.5lf %f %f Geofence: alt min: %.4f, alt_max: %.4f Geofence imported Geofence: import error Geofence import error Maximum altitude above home exceeded by %.1f m Maximum distance from home exceeded by %.1f m Geofence: %i inclusion, %i exclusion polygons, %i inclusion, %i exclusion circles, %i total vertices Engine failure. Loitering down GPS failure: request flight termination Global position failure: fixed bank loiter no GPS recovery, terminating flight terminate GPS not recovered, switching to next failure state unable to reach heading within timeout DO_SET_SERVO command Running # MIN MAX TRIM DZ REV %2d %4d %4d %4d %3d %3d input_rc callback registration failed! rc_update: cycle rc_update: cycle interval rc_update: valid data interval RC%d_MIN RC%d_TRIM RC%d_MAX RC%d_REV RC%d_DZ RC_MAP_PARAM%d channel count changed %d -> %d input source changed %d -> %d Airspeed status: CAL_AIR_CMODEL CAL_AIR_TUBELEN CAL_AIR_TUBED_MM CAL_ACC0_ID CAL_GYRO0_ID SENS_BOARD_Z_OFF SYS_PARAM_VER SYS_AUTOSTART SYS_AUTOCONFIG TRIG_MODE UAVCAN_ENABLE SYS_CAL_TDEL SYS_CAL_TMAX SYS_CAL_TMIN WARNING: failed to set scale / offsets for airspeed sensor OFF STALE TIMEOUT ERR CNT ERR DNST %s sensor switch from #%i %s #%i fail: %s%s%s%s%s! failed to add validator for sensor %s %i selected gyro: %d (%d) selected accel: %d (%d) Accel Gyro roll pitch Starting in test mode MNT_MODE_IN MNT_MODE_OUT MNT_MAV_SYSID MNT_MAV_COMPID MNT_OB_LOCK_MODE MNT_OB_NORM_MODE MNT_MAN_PITCH MNT_MAN_ROLL MNT_MAN_YAW MNT_DO_STAB MNT_RANGE_PITCH MNT_RANGE_ROLL MNT_RANGE_YAW MNT_OFF_PITCH MNT_OFF_ROLL MNT_OFF_YAW could not get mount parameters! invalid input mode %i memory allocation failed invalid output mode %i failed to initialize output mode (%i) failed to read input %i (ret: %i) failed to write output (%i) missing command mount driver already running mount driver already running, run vmount stop before 'vmount test' failed to start mount driver not running Input: None Output: None unrecognized command Input: Mavlink (ROI) Input: Mavlink (CMD_MOUNT) Input: RC (channels: roll=%i, pitch=%i, yaw=%i) Input: Test Output: Mavlink Output: AUX missing firmware filename or command setopt option bits are already set as required option control register unlock failed option bits set option bits setting failed; readback 0x%04x open %s failed stat %s failed %s: file too large (limit: %u, actual: %d) firmware read error image validated, erasing bootloader... not a bootloader image erase error at %p flashing... program error at %p verifying... verify failed at %i - retry update, DO NOT reboot bootloader update complete [%s] /fs/bbr4 Failed to open Fault Log file [%s] (%d) Failed to get Fault Log descriptor (%d) Processor registers: from 0x%08x r0:0x%08x r1:0x%08x r2:0x%08x r3:0x%08x r4:0x%08x r5:0x%08x r6:0x%08x r7:0x%08x r8:0x%08x r9:0x%08x r10:0x%08x r11:0x%08x r12:0x%08x sp:0x%08x lr:0x%08x pc:0x%08x xpsr:0x%08x basepri:0x%08x control:0x%08x exe return:0x%08x Fault status registers: from NVIC cfsr:0x%08x hfsr:0x%08x dfsr:0x%08x mmfsr:0x%08x bfsr:0x%08x afsr:0x%08x outside of within %s memory region, stack pointer lies %s stack <-- top bottom 0x%08x 0x%08x%s Interrupt sp User sp %Y-%m-%d-%H:%M:%S System fault Occurred on: %s Type:Hard Fault Type:Assertion failed in file:%s at line: %d running task: %s FW git-hash: %s Build datetime: %s %s 04:38:11 Build url: %s [%s] -- %s %s Fault Log -- Valid %s stack: top: 0x%08x sp: 0x%08x %s bottom: 0x%08x size: 0x%08x used: %08x Invalid Stack! (Corrupted TCB) Stack base: %08x Stack size: %08x Failed to re arming Fault Log (%d) Fault Log is Armed Failed to Close Fault Log (%d) Fault Log info File No %d Length %d flags:0x%02x state:%d Fault Logged on %s - Valid /fs/bbr0 Failed to open Fault reboot count file [%s] (%d) Failed to read Fault Log file [%s] (%d) Begin User Failed to re-arm Fault Log (%d) Failed to Write Fault Log (%d) Nothing to save /fs/microsd/ %Y_%m_%d_%H_%M_%S fault_%s.log Saving Fault Log file %s Done saving Fault Log file Appending to ULog %s Reading ULog header failed Cannot append more data to ULog (no offsets left) char[%i] hardfault_plain read() failed: %i, %i Successfully appended to ULog No ULog to append to Failed to append to ULog (%i) check rearm ../../src/systemcmds/hardfault_log/hardfault_log.c commit qk:v:s: query can't open %s can't reset mixers on %s can't load mixer file: %s failed to load mixers from %s missing device or filename failed to load mixer append failed to append mixer Unknown command Erasing %s Failed to open partition Erased %lu bytes Driver not running invalid instance MTD driver not started Flash Geometry of instance %i: blocksize: %lu erasesize: %lu neraseblocks: %lu No. partitions: %u partition: %u: name: %s blocks: %u (%u bytes) Device size: %u Blocks (%u bytes) TOTAL SIZE: %u KiB erase open '%s' failed (%i) importing from '%s' failed (%i) importing failed (%i) Symbols: x = used, + = saved, * = unsaved %u/%u parameters used. * symbol only allowed at end of search string <unknown type %d> <error fetching parameter %lu> SENS_BOARD_ MAV_TYPE param set %s Parameter %s not found. %c %s: curr: %ld -> new: %ld curr: %4.4f -> new: %4.4f <unknown / unsupported type %d> Parameter %s not found <unknown / unsupported type %d> param not found for index %u index %d: %c %c %s [%d,%d] : save exporting to '%s' failed (%i) Param save failed (%i) import select selected parameter default file %s show %u parameters total, %u used. show-for-airframe if [ $AUTOCNF = yes ] not enough arguments. Try 'param set PARAM_NAME 3 [fail]' compare not enough arguments. Try 'param compare PARAM_NAME 3' greater not enough arguments. Try 'param greater PARAM_NAME 3' not enough arguments (use 'param reset_all' to reset all). reset_all touch param %s not found not enough arguments. index_used no index provided index Found param %s at index %i not enough arguments. Try 'param find PARAM_NAME' d:vec:g:m:ap:r: /dev/ device %s not valid bad channel_group value BAD set_mask VAL CLI argument parsing for PWM value failed CLI argument parsing for PWM rate failed Channels: can't open %s PWM_SERVO_GET_COUNT PWM_SERVO_SET_ARM_OK Task exited with errno=%i PWM_SERVO_ARM Outputs armed disarm PWM_SERVO_DISARM Outputs disarmed oneshot PWM_SERVO_SET_UPDATE_RATE (check rate for sanity) PWM_SERVO_SET_SELECT_UPDATE_RATE PWM_SERVO_GET_RATEGROUP(%u) min: no channels set min: no PWM value provided failed get min values Channel %d: min PWM: %d min: no channels provided failed setting min values (%d) failed get max values Channel %d: max PWM: %d max: no PWM channels failed setting max values (%d) reading disarmed value of zero, disabling disarmed PWM failed get disarmed values chan %d: disarmed PWM: %d disarmed: no PWM channels failed setting disarmed values (%d) failsafe: no PWM provided failed get failsafe values Channel %d: failsafe PWM: %d failsafe: no PWM channels BAD input VAL PWM_SERVO_GET(%d) PWM_SERVO_SET(%d) User abort steps Running 5 steps. WARNING! Motors will be live in 5 seconds Press any key to abort now. Step input (0 to 100%%) over %u us ramp device: %s PWM_SERVO_GET_DEFAULT_UPDATE_RATE PWM_SERVO_GET_UPDATE_RATE PWM_SERVO_GET_SELECT_UPDATE_RATE PWM_SERVO_GET_FAILSAFE_PWM PWM_SERVO_GET_DISARMED_PWM PWM_SERVO_GET_MIN_PWM PWM_SERVO_GET_MAX_PWM PWM_SERVO_GET_TRIM_PWM channel %u: %u us (alternative rate: %d Hz (default rate: %d Hz failsafe: %d, disarmed: %d us, min: %d us, max: %d us, trim: %5.2f) %u: ERROR channel group %u: channels forcefail arg missing [on|off] FAILED setting forcefail %s terminatefail FAILED setting termination failsafe %s unlock unlock failed (%i) reboot failed (%i) once f:d:t:m:s: Start playback... Playback finished. libtest Tune ID not recognized. frequency: %d, duration %d, silence %d, volume %d Stopping playback... CROM init.d rc.uuv_apps ekf2 start & uuv_att_control land_detector rover set +e R /` AUTOCNF no X_MODE pwm` DATAMAN_OPT ""` FAILSAFE non CONFIG /fs/microsd/etc/config.tx EXTRAS extras IOFW "` /px4_io-v2_default.bin IO_PRESENT LOGGER_ARGS BUF 14` MAV_TYP MIXER BLCTRL@ OUTPUT PARAM params _DISZV ARMED p:PWM_AUX_DISA@ set OUT none RATE RC_INPUT_ARGS ""` SDCARD L XERS_PATH /fs/microsd/etc xers TARTUP_TUNE 1` USE_IO }` VEHICLE_TYPE ARA EFAULTS_VER < mount -t procfs /@ rcon ver all uorb start vfat /dev/mmcsd0 then@- hardfault_logZV check then set STARTUP_TUNE 2 f hardfault_log commit re ? [ ! -f "/fs/microsd/.metadata_ne ver_index" ]; `O cat > Trashes fs n ntsd mkdir /noA' -1000 else P_ZV TUNE 14 # tune@ = SD_INIT if mkfatfs /dev/mmcsd0 then` ount -t v # /fs/microsd echo "INFO [init] card formatted else set STARTUP_T` ERROR fail@O [ -f $FRC ] mft query -q -k MTD -s@ _PARAMETERS -v td_params _FILE CALDATA caldata load select $ import _all BZV if ver hwtypecmp V5X00@ then netman update -i eth0 param gre r SYS_AUTOCONFIG com reset_all START RC* COM_FLTMODE* LND IGHT_T_* TC CAL_AC@) GYRO `3`& UUID@ NF yes BOARD_RC_DEFAULTS ${R}etc/init.d /rc.board_defaults@ [ -f $ echo "B@6 tone!8 arm start CBRK_BUZZER 78209ZV if [ $? != 0 -o $STARTUP_TUNE@ then tune_control play -t dataman star DATAMAN_OPT send_event load_mo rgbled -X -q _ncp5623c param greater -s LIGHT_EN_BLINKM blinkm ystem com e SYS_AUTO` . ${R}etc/init.d/rc.auto K [ -f $FCONFIG echo "Custom: D }"@R CNF = yes IOFW v!( hwtypecmp ZV V540 V560 then param set SYS_USE _IO 0 else if px4io checkcrc ${I OFW} IO_PRESENT yes tune_control play -t 16 # @ = PROG_PX4IO start afety_on forceupdat c 4662 usleep 10 echo "` CRC OK after `p ing" = no ] e failed 8 HZV PROG_PX4IO_ERR if param com e -s SYS_USE_IO 1 then set -a $ a PRESENT no ] echo "` t found" tune_control play error@_ rc_update start@o gre HITL 0 OUTPUT_MODE hil nsors mand > GPS_1_CONFIG U q 4 else o t BOARD_RC_! SORS ${R}etc/init.d/rc.board_ [ -f $ B@4 nset BOARD_RC_SENSORS . ${R}etc/ init.d/rc.sensors if param com e -s BAT1_SOURCE 2 then esc_batt ery start fi@; mander P E _EN_LL40LS FMU_MODE pwm4` FD_EXT_AT@S grea TRIG PINS 56 else pwZV set AUX_MODE pwm6 else` camera_trigger start feedback if param great / -s UAVCAN_ENABLE 0 then@( uavcan OUTPUT _esc@ tune_control play error@ BOARD_RC_MAVLINK ${R}etc/init.d/ rc.board_mavlink@ [ -f $ echo "B@4 extras: T {R}etc/init.d/rc.serial if [ $IO _PRESENT = no ] then rc_input st art $RC_INPUT_ARGS . ${ vehicle_setup@_ param greater -s CAM_CAP_FBACK 0 camera_capture on@| navigator rmal <` MNT_MODE vmoun com e@7!- S_EN_PX4FLOW px4flow TEL_BST A IMU_GYRO_FF gyro_ff ?@<!} BOARD_! EXTZV RAS ${R}etc/init.d/rc.board_extr if [ -f $BOARD_RC_EXTR 7 then echo "B@2 unset Addons script@l logging@b ! param com e SYS_AUTOSTART 0 autostart.p PARAM_VER D DEFAULTS@ Switched to different eter version. Re!1 seZV t SYS_AUTOCONFIG 2 param save boot unset R X_MODE DATAMAN_OPT FAILSAF EXTRAS IO_PRESEN IOFW LOGGER_ARG MAV_TYP MIXE MKBLCTRL@n OUTPUT PARAM_DEFAULTS_V PWM@{ _DISARMED ARZV unset PWM_MAX RATE RC_INPUT_ARGS SDCARD A XERS_PATH TARTUP_TUN USE_IO VEHICLE_TYPE mavlink boot_comple rc.fw_defaults set VEHICLE_TYPE fw if [ $AUTOCN F = yes ] then param s 4 COM_POS_FS_DELAY 5 EPH 1 V 30 GAIN PROB 1 VEL@ EKF2_ARSP_THR 8 FUSE_BETA GPS_CHECK 2 MAG_ACCLIM REQ HDRIFT 0. 2ZV aram set RTL_RETURN_ALT 100 DESCEND DELAY -1 NAV_ACC_RAD 5 MIS_LTRMI TAKEOFF PWM M TE 5 GPS_UBX_DYNMO MIXER_AUX pass` rc.boat_defaults set VEHICLE_TYPE rover if [ $AUT OCNF = yes ] then param s 7 MIS_LTRMIN_ALT 0.01 TAKEOFF NAV_DLL_AC ACC_RAD 2 FW@I` 1000 PWM_OUT 1234 RATE 50` MIXER_AUX pass` rc.board_defaults set BL_FILE /etc/extras/px4fmuv3 _bl.bin if [ -f $ the` param com e SYS_ # UPDATE 1 echo "BL update..." >> $LOG`r done reboot IMU_GYRO_R MAX 400@X J [ $AUTOCNF = yes rc.interface set OUTPUT_CMD pwm_out MIXER_AUX_FILE none` DEV /dev/ put1 if param greater -s MNT_MODE_IN then com mount [ $US V O = } . Y@ @e`3 IO_PRESENT io@0 DSHO!y ONFIG dsho dshot else set OUTPUT_MODE pwm_o if [ $ != none ] then = mkblctrl MKBLCTRL ARG "-mkmode x" tune_control play error@; > } hil -o start -m _$FMU`4 echo "$ZV OUTPUT_CMD start failed" tune_co ntrol play error if [ $O MODE = uavcan_esc ] then@% param com e UAVCAN_ENABLE 0 3@h . ${R}etc/init.d/rc.io 7 IO_PRESENT 6 MIXER@8 none -a skip _AUX USE_IO FILE" 9`K -f 4 SDCARD_`* S_PATH}/ .main.mix ]ZV then set MIXER_FILE ${SDCARD_` S_PATH}/${` }.main.mix else if [ -f ix ] /etc/ $OUTPUT_MODE = mkblctrl DEV /dev/ pwm_output0 i uavcan_esc er load!_ a*aC echo "INFO [init] Mixer: ${ MIXER_FILE} on OUTPUT_DEV}" else ERROR Failed loading m tune_control play -t 18 # @ = PROG_PX4IO_ a if [ $`M != skip ] undefined _AUX@| no 1 -a $ _MODE SDCARD_`> S_PATH}/ }.aux.!, set /etc/ UXZV }.aux.mix ] then set MIXER_AUX_F ILE /etc/ " ers/${ if [ $ != none $OUTPUT_CMD mode_${@- MODE} param greater SYS_HITL 0 v append ${ DEV} echo "INFO [init] M@D ed to else ERROR Fail 1 "A, [ -e @ c loa erZV : ${MIXER_AUX_FILE} on OUTPUT` DEV}" else echo "ERROR [init] F ailed loading mixer: A set PWM` non FAILSAFE@ : Could t start: pwm_out mode_ tune_control play -t 18 # @ = PROG_PX4IO_ X` if [ $ 'A$ CMD != dsh then P !@= RATE rate -c!N } -r DISARME` then pwm disarmed -c ${PWM_AU X_OUT} -p DISARMED if [ $ MIN != none i 9 AUZV X_DEV} pwm disarmed -c 5 -p p:PW M_AUX_DIS d ${OUTPUT min@3 MIN 3ZV :PWM_AUX_MIN6 -d ${OUTPUT` DEV} pwm min -c 7 -p p: ax@3 -ZV c 8 -p p:PWM_AUX_MAX d ${OUTPUT` DEV} if [ $FAILSAFE@ != none ] then pwm failsafe -c C 7ZV -p p:PWM_AUX_FAIL7 -d ${OUTPUT` DEV} pwm failsafe -c 8 if [ $ MODE = V _out -o io ] then 7@i ! != none RATE rat` ${@% B } -r DISARMED disarmed AX`C 1@%! WMZV _MAIN_DIS1 pwm disarmed -c 2 -p p:PWM_ min@ p:ZV PWM_MAIN_MIN8 pwm max -c 1 -p p: if [ $FAILSAFE != none ] then`= failsafe@B ${@= OUT}@K PUT_DEV} pwm failsafe -c 5 -p p:PWM_MAI N_FAIL5 unset OUTPUT_CMD MIXER_AUX_FILE rc.airship_defaults set VEHICLE_TYPE airship MIXER_AUX pass` PWM@ _OUT 1234 rc.io if [ $OUTPUT_MODE = hil ] then s et HIL_ARG i`: IO_PRESENT 9 px4io start $ recovery else echo "PX4IO failed" tune_control play -t 18 # PROG_`2 _ERR@ airframes 4050_generic_250 . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 if [ $AUTOCNF = yes then param @1 MC_ROLL_P 8 RATE PITCH T YAW T `1@m MAX 160 paZV ram set MPC_MANTHR_MIN 0 _TILT `1 DL_FAC 0.3 PWM`K 1075 RATE SDLOG_PROFILE 19 IMU_DGYRO_CUTOFF 5 CBRK_IO_SAFETY 22027 3031_phantom . ${R}etc/init.d/rc.fw_defaults if [ $AUTOCNF = yes ] then param set FW_AIRSPD_MIN 13 TRIM 15 MAX 2 R_TC 0. L1_DAMPING PERIOD PR_FF 1 P_LIM` ROLL ~ R_R@D seZV t PWM_DISARMED 1000 param set SE NS_BOARD_Y_OFF 7 MIXER phantom` OUT 4 14002_tri_y_yaw- . ${R}etc/init.d/rc.mc_defaults set MIXER tri_y_yaw-` PWM_OUT 1234 13005_vtol_AAERT_quad . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set PWM_AUX_DIS5 950 RATE 40 MC_ROLL_P 6 0.17 PITCH p YAW q AWZV RATE_FF 0 param set MC_YAWR@ MAX 4 FW_PR`N I 0.02 THR_CRUISE VT_ARSP_BLEND TRANS 1 MOT_ID 4 IDLE_PWM_MC 108 TYPE 2 IXER quad_x t MIXER_AUX vtol_AAERT set PWM_O UT 1234 3035_viper . ${R}etc/init.d/rc.fw_defaults set MIXER Viper 1001_rc_quad_x.hil . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 param @ SYS_HITL 1 2106_albatross . ${R}etc/init.d/rc.fw_defaults if [ $AUTOCNF = yes ] then param set FW_AIRSPD_MIN 10 TRIM 15 MAX 2 MAN_P R_L d WR_FF 0.2 _R`+ PWM_DISARMED! MIXER AAVVTWFF` OUT 5 13200_generic_vtol_tailsitter . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set VT_ELEV_MC_LOCK 0 MOT_COUNT 2 TYPE IXER ` tailsitter_duo` PWM_OUT 1234 3000_generic_wing . ${R}etc/init.d/rc.fw_defaults set MIXER generic_wing 3033_wingwing . ${R}etc/init.d/rc.fw_defaults if [ $AUTOCNF = yes ] then param set BAT_N_CELLS 2 FW_AIRSPD_MAX 15 IN 10 TRIM 13 R_TC 0. L1_DAMPING PERIOD 16 ND_A 3 FLALT HHDIST HVIR THR` PR_FF PWM_ ARME set MAV_TYPE 1 IXER wing@ PWM_OUT 4 7001_hexa_+ . ${R}etc/init.d/rc.mc_defaults set MIXER hexa_+` PWM_OUT 12345678 8001_octo_x . ${R}etc/init.d/rc.mc_defaults set MIXER octo_x` PWM_OUT 12345678 13001_caipirinha_vtol . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set MAV_TYPE 19 C_ROLL_P 6 RATE 0.12 FF 0 PITCH p YAW p VT_IDLEZV _PWM_MC 1080 param set VT_ELEV _LOCK MOT_ID 12 TYPE * IXER vtol_tailsitter_duo` OUT S 13006_vtol_standard_delta . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set MC_ROLL_P 6.5 RATE FF 0 PITCH o YAW p MAX 5 MPZV C_XY_P 0.8 param set MPC@ VEL_P_ACC 2 _HOR_MAX YAWRAUTO PWM_AUX_DIS3 95 RATE 40 VT_MOT_ID 1234 _TRANS_THR IDLE_@t MC 108 TYPE IXER quad_x vtol_delta` OUT@ 9001_octo_+ . ${R}etc/init.d/rc.mc_defaults set MIXER octo_+` PWM_OUT 12345678 4014_s500 . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 if [ $AUTOCNF = yes then param @1 MC_ROLLRATE_P 0.18 PITCH 10017_steadidrone_qu4d . ${R}etc/init.d/rc.mc_defaults if [ $AUTOCNF = yes ] then param set BAT_N_CELLS 4 MC_ROLL_P 7 RATE 0.13 PITCH T `5`o YAW T `1@m IXER quad_w` PWM_OUT 1234 4001_quad_x . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 4010_dji_f330 . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 if [ $AUTOCNF = yes then param @1 MC_ROLL_P 7 RATE 0.15 PITCH T YAW T `3@o MINAw 13003_quad_tailsitter . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set PWM_MAX 2000 RATE 4 VT_MOT_ID 1234 IDLE_@7 MC 108 TYPE ELEV . _LOCK 1 IXER quad_x_@ OUT@ 1000_rc_fw_easystar.hil . ${R}etc/init.d/rc.fw_defaults if [ $AUTOCNF = yes ] then param set BAT_N_CELLS 3 FW_AIRSPD_MAX 20 IN 12 TRIM 14 R_TC 0. L1_DAMPING PERIOD 16 ND_A 3 FLALT HHDIST HVIR THR` PR_FF !uZV aram set FW_RR_FF 0.6 MAX RWTO_TKO ] SYS_HITL MIXER AERT 3032_skywalker_x5 . ${R}etc/init.d/rc.fw_defaults if [ $AUTOCNF = yes ] then param set FW_AIRSPD_MIN 15 TRIM 20 MAX 4 R_TC 0.3 L1_DAMPING PERIOD 16 ND_A 3 FLALT HHDIST HVIR THR` PR_FF MIXER ! generic_wing 4011_dji_f450 . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 if [ $AUTOCNF = yes then param @1 MC_ROLL_P 7 RATE 0.15 PITCH T YAW T `3@o MINAw 10015_tbs_discovery . ${R}etc/init.d/rc.mc_defaults if [ $AUTOCNF = yes ] then param set MC_ROLL_P 6.5 RATE PITCH T `8`q YAW T `4@o IXER quad_w` PWM_OUT 1234 14001_tri_y_yaw+ . ${R}etc/init.d/rc.mc_defaults set MIXER tri_y_yaw+` PWM_OUT 1234 1002_standard_vtol.hil . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set BAT_N_CELLS 3 COM_RC_IN_MODE 1 EKF2_AID_MASK NGERR 9 IT 0.0 GBIAS MAG_TYP RSP@ X 25 IN 14 TRIM 16 MC_PITCH_P RATE ROLL MIS_LTR _ALT 1 TAKEOFF YAW_ZV TMT 10 param set MPC_ACC_HOR_MAX IN 0.1 KO_SPEED XY_P 0 VEL_D@o _DN 1.5 NAV@2 _RAD DLL LOITER`2 ESCEN DELAY RETURN`6 SDLOG_DIRS@ t ZV SYS_RESTART_TYPE 2 param set VT_ F_TRANS_THR 0.75 MOT_ID 1234 HITL 1 IXER standard_vtol_hitl` PWM_OUT@i 10016_3dr_iris . ${R}etc/init.d/rc.mc_defaults if [ $AUTOCNF = yes ] then param set MC_ROLL_P 7 RATE 0.15 PITCH T YAW T `3@o BAT_V_DIV 12.27559 A_PER_ 5.39103 MIXER quad_w` PWM_OUT G 13000_generic_vtol_standard . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set PWM_AUX_DIS5 950 RATE 40 VT_TYPE 2 MOT_ID 1234 IXER quad_x AAERT` OUT@M 12001_octo_cox . ${R}etc/init.d/rc.mc_defaults set MIXER octo_cox` PWM_OUT 12345678 5001_quad_+ . ${R}etc/init.d/rc.mc_defaults set MIXER quad_+` PWM_OUT 1234 13013_deltaquad . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set BAT_CAPACITY 23000 N_CELLS 4 R_INTERNAL 0.0025 CBRK_AIRSPD_CHK 162128 IO_SAFE@w 2027 EKF2_GPS_POS_X -0.12 TAU_VE@ _GATE 1 FW_A _MOD L1_PERIOD PR_FF 0. _TC W_ZV PSP_OFF 5 param set FW_R_LIM 3 R_ * T_HRATE T_CLMB_MAX 3 SINK IN 1 VERT_ACC 6 HR_CRUISE SLEW` MAN_P PAL` _NEG 4 @e!p W_ZV BAT_SCALE_EN 1 param set FW_THR_ L 2.7 _RLL2 " LNDMC`5 MAX 9 XY_VEL` ROLL_P 6.5 RATE 0.16 PITCH _YAW_P 3.5 param set MC_ RATE MAX 2 AIRMODE IS_DIST_1WP 10 WPS@ TAKEOFF_ALT 1 PC_XY` VEL_P_ACC _HOR` LAND_SPEED 1 TILT 4 _LND 3 raZV m set MPC_HOLD_MAX_XY 0.5 param TKO_RAMP_T 0.8 XY_CRUISE ILT@R AIR 2 YAWRAUTO@ NAV_DLL_AC LOITER D 10 PWM_AUX_DISARMED 95 MAIN@ 5 15 RATE 4 SENS_BOARD_ROT 1 1_CONFIG MAZV V_1_FORWARD 1 param set SER_TEL2 _BAUD 57600 VT_TYPE 2 MOT_I G _TRANS_THR DWN_PITCH_MAX 8 QC_P 55 MIN_TM 1 WV_LND_EN FWD@ UST_SC IDLE_PWM_MC 102 REV_OUT 0. 0.7 PERM_STAB VTZV _TRANS_TIMEOUT 22 param set VT_F RAMP 4 COM_RC_OVERRIDE 0 MAV_TYPE@J` IXER deltaquad _AUX pass` PWM_@ 1234 4031_3dr_quad . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 if [ $AUTOCNF = yes then param @1 MC_ROLL_P 6.5 RATE 0.14 PITCH S YAW T 12002_steadidrone_mavrik . ${R}etc/init.d/rc.mc_defaults if [ $AUTOCNF = yes ] then param set MC_PITCH_P 4 RATE MAX 180 ROLL t YAW p PC_HOLD@~ _XY 6 THR_MIN t ZV MPC_Z_VEL_MAX_DN 2 param set BAT _N_CELLS 4 MIXER octo_cox_w` PWM_OUT 12345678 13012_convergence . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set CBRK_AIRSPD_CHK 162128 FW_A _MODE 1 L1_PERIOD 17 MAN_R X 50 ACRO_X` 27 PR_FF 0.5 P 0.0 _LIM _NEG FZV W_YR_FF param set FW@ MC_PITCHRATE_D@4 ROLL`5 U 6 YAW`5 MAX 120 @8 T MPC_LAND_SPEED 1.2 Z_VEL@ _UP PWM_@n SENS_BOARD VT_B_TRA DUR _DZV UR 1.2 param set VT_F_TR_OL_TM W_DIFTHR_EN 1 SC 0.17 MOT_OFFID 3 PERM_STAB 0 IDLE_PWM_MC 120 @R O TIL@V TRANS 0.45 _MINA P2_DUR ELEV r _LOCK YPE IXER vtol_convergence` OUT@ 1100_rc_quad_x_sih.hil . ${R}etc/init.d/rc.mc_defaults set MIXER quad_x` PWM_OUT 1234 param @ SYS_HITL 2 3036_pigeon . ${R}etc/init.d/rc.fw_defaults if [ $AUTOCNF = yes ] then param set FW_AIRSPD_MIN 15 TRIM 20 MAX 27 TT_TC 0.3 L1_DAMPING PERIOD PR_FF 1 _LIM` ROLL R_R@D amZV set FW_R_TC 0.3 param @ PWM_DISARMED 1000 SENS_BOARD_Y_OFF 11.9 MIXER phantom` OUT 4 10018_tbs_endurance . ${R}etc/init.d/rc.mc_defaults if [ $AUTOCNF = yes ] then param set BAT_N_CELLS 6 V_EMPTY 3.5 MC_ROLL_P 7 RATE 0.08 PITCH T `5@o YAW T `3@o PC_XY_VEL_MAX PWM_MIN 1080 MIXER quad_w` $ZV _OUT 1234 13007_vtol_AAVVT_quad . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set MC_ROLL_P 7 RATE 0.15 FF 0 PITCH p YAW q MAX 4 MPZV C_YAWRAUTO_MAX 40 param set PWM_ AUX_DIS5 95 RATE 0 VT_F_TRANS_THR 0.75 MOT_ID 1234 IDLE_@t MC 108 s TYPE 2 IXER quad_x vtol_AAVVT` OUT@ 6001_hexa_x . ${R}etc/init.d/rc.mc_defaults set MIXER hexa_x` PWM_OUT 12345678 11001_hexa_cox . ${R}etc/init.d/rc.mc_defaults set MIXER hexa_cox` PWM_OUT 12345678 13009_vtol_spt_ranger . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set FW_AIRSPD_MAX 22 TRIM L1_PERIOD 8 PR_P 0.060 _NEG 4 RR_FF `M 0 MC_PITCHRATE_D@6 ROLL`3 seZV t MC_ROLLRATE_I 0.002 param set MAX 60 YAW`1`l IS_TAKEOFF_ALT 2.5 _TM R PC_ACC_HOR`o HOLD@ _XY 0. LAND_SPEED MANTH r IN@9 X : ILT 6 _AIR 3 etZV MPC_TKO_SPEED 1 param set @ XY_P 0.3 VEL_MAX P_ACC YAWRAUTO`l NAV@1 _RAD PWM_AUX_REV1 DIS5 95 RATE VT_ARSP_TRANS@M _DUR 4 IDLE_@w MO@! 1234 param set VT_FW_MOT_OFFID 1234 TRANS_MIN_TM 5 TIMEOUT YPE 2 IXER quad_x _AUX vtol_AAERT` PWM_@b 13008_QuadRanger . ${R}etc/init.d/rc.vtol_default if [ $AUTOCNF = yes ] then am set FW_THR_CRUISE 65 PR_P 0.08 MIS_YA { MT 10 C_ROLL H RATE PITCH n P 3. sZV et MC_YAWRATE_P 0.6 param se MAX 4 PC_ACC_HOR` Z_VEL@ _DN 1.5 TKO_SPEED LAND UTO@Z PWM_AU o IS5 95 REV1 1 VT_ARSP_TRANS 1 BLEND _DUR THR IDL! MC 1080ZV param set VT_MOT_ID 1234 TYPE 2 IXER quad_x _AUX vtol_AAERT` PWM_OUT@a 2100_standard_plane . ${R}etc/init.d/rc.fw_defaults if [ $AUTOCNF = yes ] then param set PWM_AUX_RATE 50 MIXER AETRFG 24001_dodeca_cox set VEHICLE_TYPE mc if [ $AUTOCN F = yes ] then param s 4 NAV_ACC_RAD 2 PWM_AUX TE 400 DISARMED 9 MIN 1075 AX 195 RTL_DESCEND_ALT L DELAY RETURN`6 MIXER dodeca_top_cox bottom 2345678 rc.fw_apps ekf2 start & fw_att_control airspeed_selector land_det fixedwing rc.serial_port set SERIAL_DEV none if param com e "$PRT" 201; then@! [ "x@ _GPS1_" = V /dev/ttyS3` BAUD_PARAM@$ ]ZV ; then set SERIAL_DEV /dev/ttyS6` BAUD_PARAM@$ _TEL4_@ rc.autostart.post set AIRFRAME none if [ ${ } !=` then . /etc/init.d/airframes/ rc.mc_apps if param com e SYS_MC_EST_GROUP 1 then if att itude_estimator_q start echo "WARN [init] E LPE unsupported, EKF2 re v mended." local_position else ERROR not available. Using`l reboot `H < E ekf2 &@z mc_rate_control hover_thrust landZV _detector start multicopter rc.sensors if ! ver hwcmp AEROFC_V1 OMNIBUS _F4SD then BITCRAZE_@ YFLIE pwm_out i2c 1 10@ param com e -s SENS_EN_BATT 1 batt_smbus start -X LL40LS @@) inp ll40ls_ FD_EXT_AT@[ mappydo great! B12XX 0 b12xx <ZV art -X if param greater -s SE NS_EN_PGA460 0 then pga@ start SF1XX lightware_laser_i2c com R05 1 srf THERMAL TRANGER ng $`> PMW3901 pmw` VL53L1X vl53l1x ifZV param com e SENS_EXT_I2C_PRB 1 then ak0991 6 -X -R q start # external AK (Here2) is rotated 270 degrees y hmc5883 -T`Q ist8308 lis2mdl rm N if [ ${VEHICLE_TYPE} = fw -o vtol ] :!8 CBRK_AIRSPD_CHK 0 sdp3x_airspe! a 0x22@" e BOARD_FMUV3 ms5525 b `> else t ZV -X -q ms4525_airspeed start -` sensors` rc.thermal_cal set TEMP_CO START "" if param com e -s TC_A_ENABLE 1 then true" [ "x$ " != temperature_@n ensation start@H ALIB_ARGS SYS@" _ACCEL } -a" E N@1 GYRO _AZV RGS "${TEMP_CALIB_ARGS} -g" para m set SYS@ _GYRO 0 com BA " then [ "x$ " != temperature_@ ensation calib |@_ un@w rc.autostart set AIRFRAME none if param com e SYS_AUTOSTART 24001 then _dodeca_cox _hexa_+ 11 . 12002 _steadidr!f _mavrik _octo 1ZV 2001_octo_cox if param com e SYS_AUTOSTART 8 / then set AIRFRAME` _quad_+ _tbs_discovery M 6_3dr_iris 7_steadidrone endurance AIZV RFRAME 4001_quad_x if param c e SYS_AUTOSTART - then set AIR 10_dji_f330 4_s50 31_3dra 50_generic_2 " _rc` _x.hil _rZV c_quad_x_sih.hil if param com e SYS_AUTOSTART 14001 then set A IRFRAME _tri_y_yaw+ 3000 _generic_wing _phantom _skywalker_x5 RAZV ME 3035_viper if param com e SYS_AUTOSTART@, then set AIRFRAM`C 6_pigeon _albatross 1000 _rc_fw_easystar.hil ndard_plane vtol _generic`P RTZV 13005 then set AIRFRAME ` _vtol_AAERT_quad if param com e SYS_AUTOSTART`7 standard_delta AAVV 8_Q D Ranger spt_r 01_caipirinZV ha_vtol if param com e SYS_AUTOSTART 13200 then set A IRFRAME _generic`L _tailsitter _quad 12_conver [ ${ } != none ] . /etc/init.d/airf x else echo "ERROR [@/ ] No file matches value found in : >> $ZV LOG_FILE param set SYS_AUTOSTART tone_alarm ${TUNE_ERR} un@/ AIRFRAME rc.rover_defaults set VEHICLE_TYPE rover if [ $AUT OCNF = yes ] then param s 7 MIS_LTRMIN_ALT 0.01 TAKEOFF NAV_DLL_AC ACC_RAD 2 FW@I` 1000 PWM_OUT 1234 RATE 50` MIXER_AUX pass` rc.vehicle_setup if [ $VEHICLE_TYPE = fw ] then MIXER none set AERT param R}etc/init.d/rc.interface fw_apps@[ echo "MC mixer undefined" coax hexa_x -o IXZV ER = octo_x -o $MIXE then set MAV_TYPE 14 if [ G tri_y_yaw- 5@I param R}etc/init.d/rc.interface mc_apps@[ VEHICLE`P rover none _generic 10@/ /rZV c.rover_apps if [ $VEHICLE_TY PE = vtol ] then MIXER none echo "VTOL mixer undefined" set firefly6 quad_x_push 2@: param R}etc/init.d/rc.interface airship AVZV _TYPE ${MAV_@ R}etc/init.d/rc.interface airship_apps if [ $VEHICLE`U = uuv ] then MIXER none echo "UUV mixer undefined" set 12@/ param No autostart ID fo ekf2 rc.rover_apps ekf2 start & rover_pos_control land_detector rc.serial set PRT_F ${R}etc/init.d/rc.seri al_port GPS_2_CONFIG . $ if [ $SERIAL_DEV != none ]; t hen`> ARGS "-e r } -g p:${BAUD_PARAM}" fi`: e`y gps start -d MAV_0 @1@B@W ${i}_MODE -r RATE"@h param com e`T` FORWARD 1 faY I aram compare MAV_${i}_RADIO_CTL 1 then set` ARGS "${ } -s" mavlink start -d ${SERI AL_DEV} x@0@Q PRT`U 1_CONFIG` . $ if [ $ != none ]; -b p:${BAUD_PARAM m MODE -r RATE"@h! FORWARD IAZV L_DEV != none ]; then set MAV_AR GS "-b p:${BAUD_PARAM} -m ${i}_MODE -r RATE" if param com e`T` FORWARD 1 RADIO_CTL mavlink start -d ${SERIALA un@S PRT_GPS1_ rc.logging if param greater -s UAVCAN_ENABL then set LOGGER_BUF 6 com e SD " _MOD ARGS "${ } -e" logg!6 start -b K!% J `\ X rc.vtol_apps ekf2 start & airspeed_selector vtol_att_control mc_rate @,@ hover_thrust_estima land_det rc.board_mavlink mavlink start -d /dev/ttyACM0 rc.mc_defaults set VEHICLE_TYPE mc if [ $AUTOCN F = yes ] then param s 4 NAV_ACC_RAD 2 RTL_RETURN_ALT 30 DESCEND` DELAY PWM_MAX 195 IN F RATE 40 GPS_UBX_DYNMO c MIXER_AUX pass` _OU rc.board_sensors rgbled start -I _ncp5623c board_ad hmc5883 -T -R 4 if ! ms5611@ 5607 -s -b 1 then set BOARD_FMUV3 0@P ver hwtypecmp V30 mpu6000 else icm20608g !ZV = 0 ] then param set SENS_EN_THE RMAL 0 l3gd20 -s -b 4 -R start lsm303d ms5611 if [ $BOARD_FMUV3 = Y mpu600 3 hmc5883 -T else@ ! ver hwtypecmp V2M unAw rc.airship_apps if param com e SYS_MC_EST_GROUP 1 then if att itude_estimator_q start echo "WARN [init] E LPE unsupported, EKF2 re v mended." local_position else ERROR not available. Using`l reboot `H < E ekf2 &@z airship_ W _control land_detec d rc.vtol_defaults set VEHICLE_TYPE vtol if [ $AUTO CNF = yes ] then param s 6 IMU_GYRO_RATEMAX 400 MIS_TAKEOFF_ALT 2 YAW_TMT 1 EKF2_ARSP_THR FUSE_BETA 1 MPC_ACC_HOR_@ TKO_SPEED VEL 1 NUAL 3 XY_CRUISE _DN 1.5 JERK@ NAV` PWM_AUX TE 5 RTL_LAND_DELAY WZV V_EN 1 rc.uuv_defaults set VEHICLE_TYPE uuv if [ $AUTOC NF = yes ] then param s 5 PWM_MAX 1950 IN 10 DISARMED 1500 RATE . OUT 1234 MIXER_AUX pass` extras px4fmuv3_bl.bin @/dev/console ttyS0 armv7-m/ _hardfault.c ) X ,@t s/%s Idle Task init irq/ _unexpectedisr.c <noname> *float (null) 6 PX4IO: starting MEM: free %u, largest ERR: not enough ) d:%u s=0x%x a m=%u set debug %d config error(s) for RC%d. 8?61$#*-pw~ylkbeHOFATSZ] ).;<52 WPY^KLEBohafst}z `ur{|QV_XMJCD !&/(=:34NI@ GRU\[vqx jmdc>907"%,+ /dev/ttyS2 used %u AP RX tim eout > PWM enabled mix txt@5 reset appen E buflen@ H:!" R: %15s (@3 H + g `?@7 .`w C?wj ?@/@ ]?ZV O: %d SUMD_DECODE_STATE_UNSYNCED GOT_HEADER x LEN` (%d) DATA[%d]@* $ -- finish CRCZV 16[1]: %x [%x] SUMD_DECODE_S TATE_GOT_CRC16[2 H_TELEMETRY@1 - OK Got valid`C Packet RXLEN O Chans@ ] V ch[@ fail u _ZV cbba`_^]\[ZYXWVUTSRQONMKJIGFDBA? =;9742/-*'# i]Wb 9a&g MGiI wn>Jj #.zf +o*7 -dibouxXcseEfFgGaAn% dobxXui aAfFeEgG @;@G@3 A_@C @SA[@ @W@7 6 ` H @ mixers tilt_quad.aux.mix M: 1 S: 0 1 -1000 coax.main.mix M: 1 S: 0 1 -10 firefly6.main.mix R: 6c quad_h.main.mix R: 4h M: 1 S: 3 5 10 hexa_+.main.mix R: 6+ mount_legs.aux.mix M: 1 S: 2 0 10 & ( 0 7 quad_+.main.mix R: 4+ M: 1 S: 3 5 10 dodeca_bottom_cox.aux.mix R: 6a octo_+.main.mix R: 8+ octo_x.main.mix R: 8x generic_diff_rover.main.mix M: 2 S: 0 2 10 octo_cox_w.main.mix R: 8cw vtol_tailsitter_duo.main.mix R: 2- S: 1 0 10 mount.aux.mix M: 1 S: 2 1 10 & O deltaquad.main.mix R: 4x M: 2 S: 1 0 800 0 -1 ` `& rover_generic.main.mix M: 1 S: 0 2 10 vtol_AAVVT.aux.mix M: 2 S: 1 0 -10 2 -7 1 -8 %H`A` quad_dc.main.mix R: 4dc hexa_cox.main.mix R: 6c delta.main.mix M: 2 S: 0 3000 5@ 0 -1 1 -` Z:@I quad_w.main.mix R: 4w M: 1 S: 3 5 10 caipi.main.mix M: 2 S: 0 0 -1 1 9 Z:@I Viper.main.mix M: 2 S: 0 0 -10 1 8 Z:@I 2 %` ` `& pass.aux.mix M: 1 S: 3 5 10 claire.aux.mix M: 1 4 10 M: 2 0 75 FX79.main.mix M: 2 S: 0 0 -10 1 9@ Z:@I IO_pass.main.mix M: 1 S: 0 stampede.main.mix M: 1 S: 0 2 10 quad_x_vtol.main.mix R: 4x M: 2 S: 1 0 -500 vtol_delta.aux.mix M: 2 S: 1 0 800 0 -1 quad_s250aq.main.mix R: 4s M: 1 S: 3 5 10 octo_cox.main.mix R: 8c blade130.main.mix H: 3 T: 0 3000 6@ P: 5@ S@4`% 0 -`9@ 3054 M ?@$ v tilt_quad.main.mix M: 2 S: 0 1 10 babyshark.main.mix M: 1 0 -10 M: 2 2 -7 1 8 R: 4x phantom.main.mix M: 2 S: 0 -600 1 65 Z:@K quad_x.main.mix R: 4x M: 1 S: 3 5 10 cloudship.main.mix M: 1 S: 0 3 -1 wingwing.main.mix M: 2 S: 0 -600 1 65 Z:@K claire.main.mix R: 4x vtol_convergence.main.mix R: 3y M: 2 S: 1 4 0 -20 0 2 8 0 75 TF-AutoG2.main.mix M: 2 O: 10 !`B & hexa_x.main.mix R: 6x dodeca_top_cox.main.mix R: 6m tri_y_yaw+.main.mix R: 3y M: 1 S: 0 2 10 firefly6.aux.mix M: 1 4 0 20 -1 M: 2 0 75 1 8 ! F` AAVVTWFF_vtail.main.mix M: 2 S: 0 -10 2 7 1 -8 #F`?` -`'` rover_diff_and_servo.main.mix M: 1 S: 0 2 10 A@;@ quad_+_vtol.main.mix R: 4+ M: 2 S: 1 0 10 AAVVTWFF.main.mix M: 2 S: 0 2 -7 1 -8 %H`A` ' n` -`'` AETRFG.main.mix M: 1 S: 0 O: 5 !`C & fw_generic_wing.main.mix M: 2 S: 0 -800 1 6 Z:@K tri_y_yaw-.main.mix R: 3y M: 1 S: 0 2 -10 CCPM.main.mix M: 2 S: 0 3 10 M: 3 1 -5 0 866 AERT.main.mix M: 1 S: 0 O: 5 !`C & vectored6dof.main.mix M: 2 S: 0 2 -4000 00 +4000 0 -` vtol_AAERT.aux.mix M: 1 0 750 0 -10 AAERTWF.main.mix M: 2 S: 0 ../../platforms/nuttx/src/px4/stm/stm32_common/adc/adc.cpp Airspeed aspd_read aspd_com_err /dev/airspeed actuator_controls_%d register callback failed! mixer_module Switched to rate_ctrl work queue: %i Mixer loaded: %s Driver instance: %i Channel Configuration: Channel %i: value: %i, failsafe: %d, disarmed: %d, min: %d, max: %d Command not None mixer load failed with %d test 0 ==== test 1 : %u failures ==== test 2 unexpected ret %d/%d 8?61$#*-pw~ylkbeHOFATSZ] ' ).;<52 WPY^KLEBohafst}z ing`ur{|QV_XMJCD !&/(=:34NI@GRU\[vqx jmdc>907"%,+ Battery index must be between 1 and 9 (inclusive). Received %d. Defaulting to 1. BAT%d_V_EMPTY Could not find parameter with name %s BAT%d_V_CHARGED BAT%d_N_CELLS BAT%d_CAPACITY BAT%d_V_LOAD_DROP BAT%d_R_INTERNAL BAT%d_SOURCE BAT_LOW_THR BAT_CRIT_THR BAT_EMERGEN_THR BAT_V_EMPTY BAT_V_CHARGED BAT_N_CELLS BAT_CAPACITY BAT_V_LOAD_DROP BAT_R_INTERNAL BAT_SOURCE SYS_HAS_MAG SYS_HAS_BARO FW_ARSP_MODE RC calibration check failed PreFlightCheck SYS_MC_EST_GROUP Arming denied! Flying with USB is not safe Arming denied! Connect power module Arming denied! Check battery Arming denied! No valid mission Arming denied! Missions require a global position Arming denied! Global position required Arming denied! Home position invalid Arming denied! Press safety switch first Arming denied! Avoidance system not ready Arming denied! One or more ESCs are offline Arming denied! Vehicle is in transition state Arming denied! Vehicle is not in multicopter mode Preflight Fail: no valid data from Compass %u Preflight Fail: Compass %u uncalibrated Preflight Fail: Compass Sensor %u missing COM_ARM_MAG_ANG Preflight Fail: Compasses %d inconsistent Please check orientations and recalibrate Preflight Fail: no valid data from Accel %u Preflight Fail: Accel %u uncalibrated Preflight Fail: Accel Range, hold still on arming Preflight Fail: Accel Sensor %u missing Preflight Fail: no valid data from Gyro %u Preflight Fail: Gyro %u uncalibrated Preflight Fail: Gyro Sensor %u missing Preflight Fail: no valid data from Baro %u Preflight Fail: Baro Sensor %u missing COM_ARM_IMU_ACC COM_ARM_IMU_GYR Preflight Fail: Accel %u inconsistent - Check Cal Preflight Advice: Accel %u inconsistent - Check Cal Preflight Fail: Gyro %u inconsistent - Check Cal Preflight Advice: Gyro %u inconsistent - Check Cal Preflight Fail: Airspeed Sensor missing Preflight Fail: Airspeed Sensor stuck Preflight Fail: check Airspeed Cal or Pitot RC_MAP_TRANS_SW RC_MAP_TRANS_SW PARAMETER MISSING. Transition switch RC_MAP_TRANS_SW not set. RC ERROR: RC%d_MIN < %u. RC ERROR: RC%d_MAX > %u. RC ERROR: RC%d_TRIM < MIN (%d/%d). RC ERROR: RC%d_TRIM > MAX (%d/%d). RC ERROR: RC%d_DZ > %u. %d config error%s for %d RC channel%s. COM_POWER_COUNT Preflight Fail: Avionics Power low: %6.2f Volt CAUTION: Avionics Power low: %6.2f Volt CAUTION: Avionics Power high: %6.2f Volt Power redundancy not met: %d instead of %d system power unavailable VTOL is not supported with fmu-v2, see docs.px4.io/master/en/config/firmware.html#bootloader COM_ARM_EKF_AB COM_ARM_EKF_GB state %d: |%.8f| > %.8f + %.8f Preflight Fail: High Accelerometer Bias Preflight Fail: High Gyro Bias Preflight%s: GPS Vert Speed Drift too high Preflight%s: Estimator not using GPS Preflight%s: GPS fix too low Preflight%s: not enough GPS Satellites Preflight%s: GPS PDOP too low Preflight%s: GPS Horizontal Pos Error too high Preflight%s: GPS Vertical Pos Error too high Preflight%s: GPS Speed Accuracy too low Preflight%s: GPS Horizontal Pos Drift too high Preflight%s: GPS Vertical Pos Drift too high Preflight%s: GPS Hor Speed Drift too high Preflight%s: Poor GPS Quality COM_ARM_MAG_STR COM_ARM_EKF_HGT COM_ARM_EKF_VEL COM_ARM_EKF_POS COM_ARM_EKF_YAW Preflight Fail: heading estimate not stable Preflight Fail: horizontal velocity estimate not stable Preflight Fail: height estimate not stable Preflight Fail: strong magnetic interference detected Preflight Fail: Height estimate error Preflight Fail: Velocity estimate error Preflight Fail: Position estimate error Preflight Fail: Yaw estimate error Fail Preflight Fail: Roll failure detected Preflight Fail: Pitch failure detected Preflight Fail: Altitude failure detected Preflight Fail: Parachute failure detected Preflight Fail: ESC failure detected Failure: RTL switch engaged Failure: Kill switch engaged Failure: Landing gear switch set in UP position COM_CPU_MAX Fail: No CPU load information Fail: CPU load too high: %3.1f%% Arm auth: Requesting authorization... ArmAuthorization COM_ARM_AUTH_TO COM_ARM_AUTH_MET COM_ARM_AUTH_ID Arm auth: Authorized for the next %u seconds Arm auth: Temporarily rejected Arm auth: Denied, waypoint %i have a invalid value Arm auth: Denied by timeout in authorizer Arm auth: Denied because airspace is in use Arm auth: Denied because of bad weather Arm auth: Denied Arm auth: No response reset velocity to GPS ecl/EKF reset velocity to flow reset to vision velocity reset velocity to zero starting vision vel fusion reset position to GPS starting GPS fusion reset position to ev position reset position to last known position starting vision pos fusion bad yaw, using GPS course stopping mag use starting vision yaw fusion Yaw aligned using IMU and GPS Emergency yaw reset - mag use stopped %s buffer allocation failed aux vel IMU and output drag GPS checks passed %s hgt timeout - reset to %s Invalid hgt mode: %d vision data stopped stopping navigation GPS quality poor - stopping use GPS fusion timeout - reset to GPS GPS data stopped GPS data stopped, using only EV or OF %llu: EKF aligned, (%s hgt, IMU buf: %i, OBS buf: %i) invalid accel bias - covariance reset mag yaw fusion numerical error - covariance reset magX %s magY %s magZ %s sideslip badly conditioned - %s covariance reset GPS yaw numerical error - covariance reset airspeed badly conditioned - %s covariance reset M 2 E ] d Z O j g y ^ X8QfJ 5!/P(~! zOs}l OUHcA zu9khaGXs: ; U a ? 3T:%A Uk\<c r E! : S! T \ Z Q ? &)'p( ,8*]( )H)i)\) &C%)$ #1$1* 2l2C1 /z.c- ,C,:,x, /E0@0 -@,#+f* 4P5]6 5#5E4/3 7f889 9W:@: 8 8<7 5m5X5c5 <selecting launchmethod %d launchdetection Launch detected: enablecontrol, waiting %8.4fs until full throttle Launch detected: enablemotors (delay not activated) Launch detected: state enablemotors #Takeoff airspeed reached runway_takeoff #Climbout #Navigating to waypoint /dev/baro IMU_GYRO_RATEMAX /dev/mag %s_%s exceeded max params for block: %s controllib exceeded max children for block: %s param too long: %s error finding param: %s No Error Invalid Task Activation Failed This error is not mapped to a string or is unknown. Dummy avoidance library called! FlightTaskAutoMapper FlightTaskAuto Obstacle message received in unsupported frame %.0f CollisionPrevention no data data_validator val: %8.4f, lp: %8.4f mean dev: %8.4f RMS: %8.4f conf: %8.4f TOUT ECNT EDNST validator: best: %d, prev best: %d, failsafe: %s (%u events) sensor #%u, prio: %d, state:%s%s%s%s%s%s unable to find or subscribe to selected sensor (%d) sensor_selection callback registration failed selected sensor: %d (%d), rate: %.1f Hz estimated bias: [%.4f %.4f %.4f] vehicle_air_data: cycle failed to add validator for %s %i %s switch from #%u -> #%d %s #%i failed: %s%s%s%s%s! selected barometer: %d (%d) %d temperature offset: %.4f vehicle_gps_position: cycle selected GPS: %d IMU_INTEG_RATE updated %d -> %d %d - IMU ID: %d, accel interval: %.1f us, gyro interval: %.1f us %d - Accel ID: %d, interval: %.1f us, Gyro ID: %d, interval: %.1f us vehicle_imu: accel update interval vehicle_imu: accel data gap vehicle_imu: gyro update interval vehicle_imu: gyro data gap vehicle_magnetometer: cycle CAL_%s%u_ID CAL_%s%u_ROT selected magnetometer: %d (%d) %s %d EN: %d, offset: [%.4f %.4f %.4f] scale: [%.4f %.4f %.4f] sensor_calibration %s %d temperature offset: [%.4f %.4f %.4f] External %s %d (%d) invalid rotation %d, resetting to rotation none Internal %s %d (%d) invalid rotation %d, resetting %s %d (%d) invalid priority %d, resetting to %d %s %d EN: %d, offset: [%.4f %.4f %.4f] %s %d EN: %d, offset: [% 05.3f % 05.3f % 05.3f], scale: [% 05.3f % 05.3f % 05.3f], External ROT: %d %s %d EN: %d, offset: [% 05.3f % 05.3f % 05.3f], scale: [% 05.3f % 05.3f % 05.3f], Internal CAL_%s%u_%s failed to get %s failed to set %s = %d CAL_%s%u_%c%s failed to set %s = %.4f invalid SENS_BOARD_ROT: %d localhost v1.11.0-rc3-889-gac99dc9a06-dirty pr-dhcp v10.0.0.0 bc0e6e37bfc1eea450ba371ee515b43999e2c5b1 GNU GCC 9.3.1 20200408 (release) ac99dc9a06c01448d46f7e324a2fbacbc9b05494 file not found line too long H: %u%n T: %u %u %u %u %u P: %d %d %d %d %d S: %u %u %d %d %d %d R: %15s 4xcw 4x1p C?wj O: %d %d %d %d %d %n S: %u %u %d %d %d %d %d M: %u%n MFT240L8 O4aO5dc O4aO5dc O4aO5dc L16dcdcdcdc MBT200a8a8a8PaaaP MFT200e8a8a MFT200e8e MFT200e8c8e8c8e8c8 MNT75L1O2G MBNT100a8 MBNT255a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8a8 MFT255L4AAAL1F# MFT255L4<<<BAP MFT255L16agagagag MFT100a8 MFT100L4>G#6A#6B#4 MFAGPAG MNBG MLL32CP8MB MLL8CDE ML<<CP4CP4CP4CP4CP4 reset done, %d ms Pixhack V3 detected, forcing to fmu-v3 bad version detected, forcing to fmu-v2 FMUv2 ver 0x%1X : Rev %x %s DMA alloc FAILED [boot] FAILED to initialize SPI port %d [boot] Failed to initialize SDIO slot %d [boot] Failed to bind SDIO to the MMC/SD driver: %d [boot] Board %4x is not supported! - Boot halted Due to Key Press /fs/bbr [boot] There is a hard fault logged. Hold down the SPACE BAR, while booting to review! [boot] There were %d reboots with Hard fault that were not committed to disk%s Enter B - Continue booting Enter C - Clear the fault log Enter D - Dump fault log Memory wiped - dump not saved! dma_alloc %4s %-*s %8s %6s %11s %10s %-5s %2s PRIO(BASE) USED/STACK CPU(%) CPU(ms) %4d %-*s %8d %6.3f %5u/%5u %3u (%3u) %-5s %2d Processes: %d total, %d running, %d sleeping, max FDs: %d CPU usage: %.2f%% tasks, %.2f%% sched, %.2f%% idle DMA Memory: %d total, %d used %d peak Uptime: %.3fs total, %.3fs idle PEND READY inact w:sem w:sig /dev/console_buf mtd->ioctl failed: %d PX4_MTD failed to allocate memory! Misconfiguration PX4_I2C_BUS_MTD not set failed to locate spi bus mtd needed %d attempts to attach failed to initialize mtd driver failed to set bus speed mtd_partition failed. offset=%lu nblocks=%lu ftl_initialize %s failed: %d bchdev_register %s failed: %d mtd failure: %d bus %d address %d class %d MTD_PARAMETERS MTD_WAYPOINTS MTD_CALDATA MTD_MFT MTD_ID MTD_NET /fs/mtd_params /fs/mtd_waypoints Running on %s Bus %i SPI_I2C Bug: driver %s does not set default_i2c_frequency Bug: driver %s does not set default_spi_frequency conflicting option: %c too many options Module did not respond to stop request Not running (external) need to specify a bus type Already running on bus %i Bug: driver %s does not pass the I2C address to I2CSPIDriverBase %s #%i on I2C bus %d%s %s #%i on SPI bus %d (devid=0x%x) (external, equal to '-b %i') %s: no instance started (no device on bus?) param name '%s' not found Reboot NOW. board shutdown not available unmatched number of px4_shutdown_unlock() calls %-5s initialized uORB logging failed to advertise log_message [32m [33m [31m DEBUG WARN PANIC %s%u %-26s %8.1f Hz %12.0f us (%lld us) %s not available px4_work_queue %-26s %8.1f Hz %12.0f us <single_shot> failed to create %s no INS%d wq configuration, using INS0 wq:manager task start failed (%i) attr init for %s failed (%i) getting sched param for %s failed (%i) setting stack size for %s failed (%i) failed to set sched policy SCHED_FIFO (%i) setting sched params for %s failed (%i) failed to create thread for %s (%i): %s failed to destroy thread attributes for %s (%i) wq:UART_UNKNOWN wq:UART8 wq:UART7 wq:UART6 wq:UART5 wq:UART4 wq:UART3 wq:UART2 wq:UART1 wq:UART0 wq:INS3 wq:INS2 wq:INS1 wq:I2C4 wq:I2C3 wq:I2C2 wq:I2C1 wq:I2C0 wq:SPI6 wq:SPI5 wq:SPI4 wq:SPI3 wq:SPI2 wq:SPI1 wq:SPI0 %s failed to init I2C %s FAIL: too slow for bus #%u: %u KHz, device max: %u KHz) %s probe failed %s cdev init failed %s on I2C bus %d at 0x%02x (bus: %u KHz, max: %u KHz) I2C device not opened drivers__device %s transfer out %p/%u in %p/%u %s I2C transfer failed, result %d %s failed to init SPI %s on SPI bus %d at %d (%u KHz) ../../platforms/nuttx/src/px4/stm/stm32_common/spi/spi.cpp decoder init failed param_export param_find param_get param_set ignoring unrecognised parameter '%s' unexpected type for %s unexpected subtype for %s bad size for '%s' failed allocating for '%s' failed copying data for '%s' /eeprom/parameters px4_shutdown_lock() failed (%i) BSON append failed for '%s' unrecognized parameter type bson encoder finish failed failed to open param file: %s param_export failed, retrying %d failed to write parameters to file: %s param auto save failed (%i) open '%s' for reading failed error reading parameters from '%s' summary: %d/%d (used/total) storage array: %d/%d elements (%zu bytes total) auto save: %s last auto save: %.3f seconds ago CAL_ACC0_EN CAL_ACC1_EN CAL_ACC2_EN CAL_GYRO0_EN CAL_GYRO1_EN CAL_GYRO2_EN CAL_MAG0_EN CAL_MAG1_EN CAL_MAG2_EN CAL_MAG3_EN CAL_MAG0_ID TC_A0_ID TC_B0_ID TC_G0_ID CAL_ACC1_ID CAL_GYRO1_ID CAL_MAG1_ID TC_A1_ID TC_B1_ID TC_G1_ID CAL_ACC2_ID CAL_GYRO2_ID CAL_MAG2_ID TC_A2_ID TC_B2_ID TC_G2_ID migrating %s (removed) -> %s: new value=%.3f COM_ARM_AUTH migrating COM_ARM_AUTH: %d -> COM_ARM_AUTH_ID:%d, COM_ARM_AUTH_MET: %d and COM_ARM_AUTH_TO: %f MPC_XY_VEL_P MPC_XY_VEL_I MPC_XY_VEL_D MPC_Z_VEL_P MPC_Z_VEL_I MPC_Z_VEL_D MC_DTERM_CUTOFF IMU_DGYRO_CUTOFF param migrating MC_DTERM_CUTOFF (removed) -> IMU_DGYRO_CUTOFF: value=%.3f EKF2_GPS_MASK SENS_GPS_MASK copying %s -> %s EKF2_GPS_TAU SENS_GPS_TAU param modify: %s, value=0x%x (old=0x%x) ASPD_BETA_GATE ASPD_BETA_NOISE ASPD_DO_CHECKS ASPD_FALLBACK ASPD_FS_INNOV ASPD_FS_INTEG ASPD_FS_T1 ASPD_FS_T2 ASPD_PRIMARY ASPD_SCALE ASPD_SCALE_EST ASPD_SC_P_NOISE ASPD_STALL ASPD_TAS_GATE ASPD_TAS_NOISE ASPD_W_P_NOISE BAT1_A_PER_V BAT1_CAPACITY BAT1_I_CHANNEL BAT1_N_CELLS BAT1_R_INTERNAL BAT1_SOURCE BAT1_V_CHANNEL BAT1_V_CHARGED BAT1_V_DIV BAT1_V_EMPTY BAT1_V_LOAD_DROP BAT2_A_PER_V BAT2_CAPACITY BAT2_I_CHANNEL BAT2_N_CELLS BAT2_R_INTERNAL BAT2_SOURCE BAT2_V_CHANNEL BAT2_V_CHARGED BAT2_V_DIV BAT2_V_EMPTY BAT2_V_LOAD_DROP CAL_ACC0_PRIO CAL_ACC0_ROT CAL_ACC0_XOFF CAL_ACC0_XSCALE CAL_ACC0_YOFF CAL_ACC0_YSCALE CAL_ACC0_ZOFF CAL_ACC0_ZSCALE CAL_ACC1_PRIO CAL_ACC1_ROT CAL_ACC1_XOFF CAL_ACC1_XSCALE CAL_ACC1_YOFF CAL_ACC1_YSCALE CAL_ACC1_ZOFF CAL_ACC1_ZSCALE CAL_ACC2_PRIO CAL_ACC2_ROT CAL_ACC2_XOFF CAL_ACC2_XSCALE CAL_ACC2_YOFF CAL_ACC2_YSCALE CAL_ACC2_ZOFF CAL_ACC2_ZSCALE CAL_ACC3_ID CAL_ACC3_PRIO CAL_ACC3_ROT CAL_ACC3_XOFF CAL_ACC3_XSCALE CAL_ACC3_YOFF CAL_ACC3_YSCALE CAL_ACC3_ZOFF CAL_ACC3_ZSCALE CAL_GYRO0_PRIO CAL_GYRO0_ROT CAL_GYRO0_XOFF CAL_GYRO0_YOFF CAL_GYRO0_ZOFF CAL_GYRO1_PRIO CAL_GYRO1_ROT CAL_GYRO1_XOFF CAL_GYRO1_YOFF CAL_GYRO1_ZOFF CAL_GYRO2_PRIO CAL_GYRO2_ROT CAL_GYRO2_XOFF CAL_GYRO2_YOFF CAL_GYRO2_ZOFF CAL_GYRO3_ID CAL_GYRO3_PRIO CAL_GYRO3_ROT CAL_GYRO3_XOFF CAL_GYRO3_YOFF CAL_GYRO3_ZOFF CAL_MAG0_PRIO CAL_MAG0_ROT CAL_MAG0_XCOMP CAL_MAG0_XODIAG CAL_MAG0_XOFF CAL_MAG0_XSCALE CAL_MAG0_YCOMP CAL_MAG0_YODIAG CAL_MAG0_YOFF CAL_MAG0_YSCALE CAL_MAG0_ZCOMP CAL_MAG0_ZODIAG CAL_MAG0_ZOFF CAL_MAG0_ZSCALE CAL_MAG1_PRIO CAL_MAG1_ROT CAL_MAG1_XCOMP CAL_MAG1_XODIAG CAL_MAG1_XOFF CAL_MAG1_XSCALE CAL_MAG1_YCOMP CAL_MAG1_YODIAG CAL_MAG1_YOFF CAL_MAG1_YSCALE CAL_MAG1_ZCOMP CAL_MAG1_ZODIAG CAL_MAG1_ZOFF CAL_MAG1_ZSCALE CAL_MAG2_PRIO CAL_MAG2_ROT CAL_MAG2_XCOMP CAL_MAG2_XODIAG CAL_MAG2_XOFF CAL_MAG2_XSCALE CAL_MAG2_YCOMP CAL_MAG2_YODIAG CAL_MAG2_YOFF CAL_MAG2_YSCALE CAL_MAG2_ZCOMP CAL_MAG2_ZODIAG CAL_MAG2_ZOFF CAL_MAG2_ZSCALE CAL_MAG3_ID CAL_MAG3_PRIO CAL_MAG3_ROT CAL_MAG3_XCOMP CAL_MAG3_XODIAG CAL_MAG3_XOFF CAL_MAG3_XSCALE CAL_MAG3_YCOMP CAL_MAG3_YODIAG CAL_MAG3_YOFF CAL_MAG3_YSCALE CAL_MAG3_ZCOMP CAL_MAG3_ZODIAG CAL_MAG3_ZOFF CAL_MAG3_ZSCALE CAL_MAG_COMP_TYP CBRK_AIRSPD_CHK CBRK_ENGINEFAIL CBRK_RATE_CTRL CBRK_SUPPLY_CHK CBRK_USB_CHK CBRK_VELPOSERR CBRK_VTOLARMING COM_ARM_AUTH_REQ COM_ARM_CHK_ESCS COM_ARM_MIS_REQ COM_ARM_SWISBTN COM_ARM_WO_GPS COM_DISARM_LAND COM_DISARM_PRFLT COM_DL_LOSS_T COM_EF_C2T COM_EF_THROT COM_EF_TIME COM_FLTMODE1 COM_FLTMODE2 COM_FLTMODE3 COM_FLTMODE4 COM_FLTMODE5 COM_FLTMODE6 COM_FLT_PROFILE COM_HLDL_LOSS_T COM_HLDL_REG_T COM_HOME_H_T COM_HOME_IN_AIR COM_HOME_V_T COM_KILL_DISARM COM_LKDOWN_TKO COM_LOW_BAT_ACT COM_MOT_TEST_EN COM_OBL_ACT COM_OBL_RC_ACT COM_OBS_AVOID COM_OF_LOSS_T COM_POSCTL_NAVL COM_POS_FS_DELAY COM_POS_FS_EPH COM_POS_FS_EPV COM_POS_FS_GAIN COM_POS_FS_PROB COM_PREARM_MODE COM_RC_ARM_HYST COM_RC_IN_MODE COM_RC_LOSS_T COM_RC_OVERRIDE COM_RC_STICK_OV COM_REARM_GRACE COM_TAKEOFF_ACT COM_VEL_FS_EVH CP_DELAY CP_DIST CP_GO_NO_DATA CP_GUIDE_ANG EKF2_ABIAS_INIT EKF2_ABL_ACCLIM EKF2_ABL_GYRLIM EKF2_ABL_LIM EKF2_ABL_TAU EKF2_ACC_B_NOISE EKF2_ACC_NOISE EKF2_AID_MASK EKF2_ANGERR_INIT EKF2_ARSP_THR EKF2_ASPD_MAX EKF2_ASP_DELAY EKF2_AVEL_DELAY EKF2_BARO_DELAY EKF2_BARO_GATE EKF2_BARO_NOISE EKF2_BCOEF_X EKF2_BCOEF_Y EKF2_BETA_GATE EKF2_BETA_NOISE EKF2_DECL_TYPE EKF2_DRAG_NOISE EKF2_EAS_NOISE EKF2_EVA_NOISE EKF2_EVP_GATE EKF2_EVP_NOISE EKF2_EVV_GATE EKF2_EVV_NOISE EKF2_EV_DELAY EKF2_EV_NOISE_MD EKF2_EV_POS_X EKF2_EV_POS_Y EKF2_EV_POS_Z EKF2_FUSE_BETA EKF2_GBIAS_INIT EKF2_GND_EFF_DZ EKF2_GND_MAX_HGT EKF2_GPS_CHECK EKF2_GPS_DELAY EKF2_GPS_POS_X EKF2_GPS_POS_Y EKF2_GPS_POS_Z EKF2_GPS_P_GATE EKF2_GPS_P_NOISE EKF2_GPS_V_GATE EKF2_GPS_V_NOISE EKF2_GSF_TAS EKF2_GYR_B_NOISE EKF2_GYR_NOISE EKF2_HDG_GATE EKF2_HEAD_NOISE EKF2_HGT_MODE EKF2_IMU_POS_X EKF2_IMU_POS_Y EKF2_IMU_POS_Z EKF2_MAGBIAS_ID EKF2_MAGBIAS_X EKF2_MAGBIAS_Y EKF2_MAGBIAS_Z EKF2_MAGB_K EKF2_MAGB_VREF EKF2_MAG_ACCLIM EKF2_MAG_B_NOISE EKF2_MAG_CHECK EKF2_MAG_DECL EKF2_MAG_DELAY EKF2_MAG_E_NOISE EKF2_MAG_GATE EKF2_MAG_NOISE EKF2_MAG_TYPE EKF2_MAG_YAWLIM EKF2_MIN_OBS_DT EKF2_MIN_RNG EKF2_MOVE_TEST EKF2_MULTI_IMU EKF2_MULTI_MAG EKF2_NOAID_NOISE EKF2_NOAID_TOUT EKF2_OF_DELAY EKF2_OF_GATE EKF2_OF_N_MAX EKF2_OF_N_MIN EKF2_OF_POS_X EKF2_OF_POS_Y EKF2_OF_POS_Z EKF2_OF_QMIN EKF2_PCOEF_XN EKF2_PCOEF_XP EKF2_PCOEF_YN EKF2_PCOEF_YP EKF2_PCOEF_Z EKF2_REQ_EPH EKF2_REQ_EPV EKF2_REQ_GPS_H EKF2_REQ_HDRIFT EKF2_REQ_NSATS EKF2_REQ_PDOP EKF2_REQ_SACC EKF2_REQ_VDRIFT EKF2_RNG_AID EKF2_RNG_A_HMAX EKF2_RNG_A_IGATE EKF2_RNG_A_VMAX EKF2_RNG_DELAY EKF2_RNG_GATE EKF2_RNG_NOISE EKF2_RNG_PITCH EKF2_RNG_POS_X EKF2_RNG_POS_Y EKF2_RNG_POS_Z EKF2_RNG_SFE EKF2_SEL_ERR_RED EKF2_SEL_IMU_ACC EKF2_SEL_IMU_ANG EKF2_SEL_IMU_RAT EKF2_SEL_IMU_VEL EKF2_TAS_GATE EKF2_TAU_POS EKF2_TAU_VEL EKF2_TERR_GRAD EKF2_TERR_MASK EKF2_TERR_NOISE EKF2_WIND_NOISE FD_ESCS_EN FD_EXT_ATS_EN FD_EXT_ATS_TRIG FD_FAIL_P FD_FAIL_P_TTRI FD_FAIL_R FD_FAIL_R_TTRI FW_ACRO_X_MAX FW_ACRO_Y_MAX FW_ACRO_Z_MAX FW_AIRSPD_MIN FW_AIRSPD_TRIM FW_ARSP_SCALE_EN FW_BAT_SCALE_EN FW_CLMBOUT_DIFF FW_DTRIM_P_FLPS FW_DTRIM_P_VMAX FW_DTRIM_P_VMIN FW_DTRIM_R_FLPS FW_DTRIM_R_VMAX FW_DTRIM_R_VMIN FW_DTRIM_Y_VMAX FW_DTRIM_Y_VMIN FW_FLAPERON_SCL FW_FLAPS_LND_SCL FW_FLAPS_SCL FW_FLAPS_TO_SCL FW_GND_SPD_MIN FW_L1_DAMPING FW_L1_PERIOD FW_L1_R_SLEW_MAX FW_LND_AIRSPD_SC FW_LND_ANG FW_LND_EARLYCFG FW_LND_FLALT FW_LND_FL_PMAX FW_LND_FL_PMIN FW_LND_HHDIST FW_LND_HVIRT FW_LND_THRTC_SC FW_LND_TLALT FW_LND_USETER FW_MAN_P_MAX FW_MAN_R_MAX FW_POSCTL_INV_ST FW_PR_FF FW_PR_I FW_PR_IMAX FW_PR_P FW_PSP_OFF FW_P_LIM_MAX FW_P_LIM_MIN FW_P_RMAX_NEG FW_P_RMAX_POS FW_P_TC FW_RATT_TH FW_RLL_TO_YAW_FF FW_RR_FF FW_RR_I FW_RR_IMAX FW_RR_P FW_RSP_OFF FW_R_LIM FW_R_RMAX FW_R_TC FW_THR_ALT_SCL FW_THR_CRUISE FW_THR_IDLE FW_THR_LND_MAX FW_THR_MAX FW_THR_MIN FW_THR_SLEW_MAX FW_T_CLMB_MAX FW_T_HRATE_FF FW_T_HRATE_P FW_T_INTEG_GAIN FW_T_PTCH_DAMP FW_T_RLL2THR FW_T_SINK_MAX FW_T_SINK_MIN FW_T_SPDWEIGHT FW_T_SPD_OMEGA FW_T_SRATE_P FW_T_THRO_CONST FW_T_THR_DAMP FW_T_TIME_CONST FW_T_VERT_ACC FW_WR_FF FW_WR_I FW_WR_IMAX FW_WR_P FW_W_EN FW_W_RMAX FW_YR_FF FW_YR_I FW_YR_IMAX FW_YR_P FW_Y_RMAX GF_ACTION GF_ALTMODE GF_COUNT GF_MAX_HOR_DIST GF_MAX_VER_DIST GF_SOURCE GPS_1_CONFIG GPS_1_PROTOCOL GPS_2_CONFIG GPS_2_PROTOCOL HTE_ACC_GATE HTE_HT_ERR_INIT HTE_HT_NOISE IMU_ACCEL_CUTOFF IMU_GYRO_CUTOFF IMU_GYRO_NF_BW IMU_GYRO_NF_FREQ IMU_INTEG_RATE LAUN_ALL_ON LAUN_CAT_A LAUN_CAT_MDEL LAUN_CAT_PMAX LAUN_CAT_T LNDFW_AIRSPD_MAX LNDFW_VEL_XY_MAX LNDFW_VEL_Z_MAX LNDFW_XYACC_MAX LNDMC_ALT_MAX LNDMC_ROT_MAX LNDMC_XY_VEL_MAX LNDMC_Z_VEL_MAX LND_FLIGHT_T_HI LND_FLIGHT_T_LO MAV_0_CONFIG MAV_0_FORWARD MAV_0_MODE MAV_0_RADIO_CTL MAV_0_RATE MAV_1_CONFIG MAV_1_FORWARD MAV_1_MODE MAV_1_RADIO_CTL MAV_1_RATE MAV_2_CONFIG MAV_2_FORWARD MAV_2_MODE MAV_2_RADIO_CTL MAV_2_RATE MAV_BROADCAST MAV_FWDEXTSP MAV_HASH_CHK_EN MAV_HB_FORW_EN MAV_ODOM_LP MAV_PROTO_VER MAV_RADIO_TOUT MAV_SIK_RADIO_ID MAV_USEHILGPS MC_ACRO_EXPO MC_ACRO_EXPO_Y MC_ACRO_P_MAX MC_ACRO_R_MAX MC_ACRO_SUPEXPO MC_ACRO_SUPEXPOY MC_ACRO_Y_MAX MC_BAT_SCALE_EN MC_MAN_TILT_TAU MC_PITCHRATE_D MC_PITCHRATE_FF MC_PITCHRATE_I MC_PITCHRATE_K MC_PITCHRATE_MAX MC_PITCHRATE_P MC_PITCH_P MC_PR_INT_LIM MC_RATT_TH MC_ROLLRATE_D MC_ROLLRATE_FF MC_ROLLRATE_I MC_ROLLRATE_K MC_ROLLRATE_MAX MC_ROLLRATE_P MC_ROLL_P MC_RR_INT_LIM MC_YAWRATE_D MC_YAWRATE_FF MC_YAWRATE_I MC_YAWRATE_K MC_YAWRATE_MAX MC_YAWRATE_P MC_YAW_P MC_YAW_WEIGHT MC_YR_INT_LIM MIS_DIST_1WP MIS_DIST_WPS MIS_LTRMIN_ALT MIS_MNT_YAW_CTL MIS_TAKEOFF_ALT MIS_TAKEOFF_REQ MIS_YAW_ERR MIS_YAW_TMT MOT_ORDERING MPC_ACC_DOWN_MAX MPC_ACC_HOR_MAX MPC_ACC_UP_MAX MPC_ALT_MODE MPC_DEC_HOR_SLOW MPC_HOLD_DZ MPC_HOLD_MAX_XY MPC_HOLD_MAX_Z MPC_JERK_AUTO MPC_JERK_MAX MPC_JERK_MIN MPC_LAND_ALT1 MPC_LAND_ALT2 MPC_LAND_RC_HELP MPC_LAND_VEL_XY MPC_MAN_TILT_MAX MPC_MAN_Y_MAX MPC_MAN_Y_TAU MPC_POS_MODE MPC_SPOOLUP_TIME MPC_THR_CURVE MPC_THR_MAX MPC_TILTMAX_AIR MPC_TILTMAX_LND MPC_TKO_RAMP_T MPC_TKO_SPEED MPC_VELD_LP MPC_VEL_MANUAL MPC_XY_MAN_EXPO MPC_XY_P MPC_XY_TRAJ_P MPC_XY_VEL_D_ACC MPC_XY_VEL_I_ACC MPC_XY_VEL_MAX MPC_XY_VEL_P_ACC MPC_YAWRAUTO_MAX MPC_YAW_EXPO MPC_YAW_MODE MPC_Z_MAN_EXPO MPC_Z_P MPC_Z_VEL_D_ACC MPC_Z_VEL_I_ACC MPC_Z_VEL_MAX_DN MPC_Z_VEL_MAX_UP MPC_Z_VEL_P_ACC NAV_ACC_RAD NAV_AH_ALT NAV_AH_LAT NAV_AH_LON NAV_DLL_ACT NAV_FORCE_VT NAV_FT_DST NAV_FT_FS NAV_FT_RS NAV_FW_ALTL_RAD NAV_FW_ALT_RAD NAV_GPSF_LT NAV_GPSF_P NAV_GPSF_R NAV_GPSF_TR NAV_LOITER_RAD NAV_MC_ALT_RAD NAV_MIN_FT_HT NAV_RCL_ACT NAV_TRAFF_AVOID NAV_TRAFF_A_RADM NAV_TRAFF_A_RADU PLD_BTOUT PLD_FAPPR_ALT PLD_HACC_RAD PLD_MAX_SRCH PLD_SRCH_ALT PLD_SRCH_TOUT PWM_AUX_DIS1 PWM_AUX_DIS2 PWM_AUX_DIS3 PWM_AUX_DIS4 PWM_AUX_DIS5 PWM_AUX_DIS6 PWM_AUX_DIS7 PWM_AUX_DIS8 PWM_AUX_DISARMED PWM_AUX_FAIL1 PWM_AUX_FAIL2 PWM_AUX_FAIL3 PWM_AUX_FAIL4 PWM_AUX_FAIL5 PWM_AUX_FAIL6 PWM_AUX_FAIL7 PWM_AUX_FAIL8 PWM_AUX_MAX PWM_AUX_MAX1 PWM_AUX_MAX2 PWM_AUX_MAX3 PWM_AUX_MAX4 PWM_AUX_MAX5 PWM_AUX_MAX6 PWM_AUX_MAX7 PWM_AUX_MAX8 PWM_AUX_MIN PWM_AUX_MIN1 PWM_AUX_MIN2 PWM_AUX_MIN3 PWM_AUX_MIN4 PWM_AUX_MIN5 PWM_AUX_MIN6 PWM_AUX_MIN7 PWM_AUX_MIN8 PWM_AUX_RATE PWM_AUX_REV1 PWM_AUX_REV2 PWM_AUX_REV3 PWM_AUX_REV4 PWM_AUX_REV5 PWM_AUX_REV6 PWM_AUX_REV7 PWM_AUX_REV8 PWM_AUX_TRIM1 PWM_AUX_TRIM2 PWM_AUX_TRIM3 PWM_AUX_TRIM4 PWM_AUX_TRIM5 PWM_AUX_TRIM6 PWM_AUX_TRIM7 PWM_AUX_TRIM8 PWM_DISARMED PWM_MAIN_DIS1 PWM_MAIN_DIS2 PWM_MAIN_DIS3 PWM_MAIN_DIS4 PWM_MAIN_DIS5 PWM_MAIN_DIS6 PWM_MAIN_DIS7 PWM_MAIN_DIS8 PWM_MAIN_FAIL1 PWM_MAIN_FAIL2 PWM_MAIN_FAIL3 PWM_MAIN_FAIL4 PWM_MAIN_FAIL5 PWM_MAIN_FAIL6 PWM_MAIN_FAIL7 PWM_MAIN_FAIL8 PWM_MAIN_MAX1 PWM_MAIN_MAX2 PWM_MAIN_MAX3 PWM_MAIN_MAX4 PWM_MAIN_MAX5 PWM_MAIN_MAX6 PWM_MAIN_MAX7 PWM_MAIN_MAX8 PWM_MAIN_MIN1 PWM_MAIN_MIN2 PWM_MAIN_MIN3 PWM_MAIN_MIN4 PWM_MAIN_MIN5 PWM_MAIN_MIN6 PWM_MAIN_MIN7 PWM_MAIN_MIN8 PWM_MAIN_REV1 PWM_MAIN_REV2 PWM_MAIN_REV3 PWM_MAIN_REV4 PWM_MAIN_REV5 PWM_MAIN_REV6 PWM_MAIN_REV7 PWM_MAIN_REV8 PWM_MAIN_TRIM1 PWM_MAIN_TRIM2 PWM_MAIN_TRIM3 PWM_MAIN_TRIM4 PWM_MAIN_TRIM5 PWM_MAIN_TRIM6 PWM_MAIN_TRIM7 PWM_MAIN_TRIM8 PWM_RATE RC10_DZ RC10_MAX RC10_MIN RC10_REV RC10_TRIM RC11_DZ RC11_MAX RC11_MIN RC11_REV RC11_TRIM RC12_DZ RC12_MAX RC12_MIN RC12_REV RC12_TRIM RC13_DZ RC13_MAX RC13_MIN RC13_REV RC13_TRIM RC14_DZ RC14_MAX RC14_MIN RC14_REV RC14_TRIM RC15_DZ RC15_MAX RC15_MIN RC15_REV RC15_TRIM RC16_DZ RC16_MAX RC16_MIN RC16_REV RC16_TRIM RC17_DZ RC17_MAX RC17_MIN RC17_REV RC17_TRIM RC18_DZ RC18_MAX RC18_MIN RC18_REV RC18_TRIM RC1_DZ RC1_MAX RC1_MIN RC1_REV RC1_TRIM RC2_DZ RC2_MAX RC2_MIN RC2_REV RC2_TRIM RC3_DZ RC3_MAX RC3_MIN RC3_REV RC3_TRIM RC4_DZ RC4_MAX RC4_MIN RC4_REV RC4_TRIM RC5_DZ RC5_MAX RC5_MIN RC5_REV RC5_TRIM RC6_DZ RC6_MAX RC6_MIN RC6_REV RC6_TRIM RC7_DZ RC7_MAX RC7_MIN RC7_REV RC7_TRIM RC8_DZ RC8_MAX RC8_MIN RC8_REV RC8_TRIM RC9_DZ RC9_MAX RC9_MIN RC9_REV RC9_TRIM RC_ACRO_TH RC_ARMSWITCH_TH RC_ASSIST_TH RC_AUTO_TH RC_CHAN_CNT RC_GEAR_TH RC_KILLSWITCH_TH RC_LOITER_TH RC_MAN_TH RC_MAP_ACRO_SW RC_MAP_AUX4 RC_MAP_AUX5 RC_MAP_AUX6 RC_MAP_FAILSAFE RC_MAP_FLTMODE RC_MAP_GEAR_SW RC_MAP_KILL_SW RC_MAP_LOITER_SW RC_MAP_MAN_SW RC_MAP_OFFB_SW RC_MAP_PARAM1 RC_MAP_PARAM2 RC_MAP_PARAM3 RC_MAP_POSCTL_SW RC_MAP_RATT_SW RC_MAP_RETURN_SW RC_MAP_STAB_SW RC_OFFB_TH RC_POSCTL_TH RC_RATT_TH RC_RETURN_TH RC_STAB_TH RC_TRANS_TH RTL_CONE_ANG RTL_DESCEND_ALT RTL_LAND_DELAY RTL_MIN_DIST RTL_PLD_MD RTL_RETURN_ALT RTL_TYPE RWTO_AIRSPD_SCL RWTO_HDG RWTO_MAX_PITCH RWTO_MAX_ROLL RWTO_MAX_THR RWTO_NAV_ALT RWTO_PSP RWTO_RAMP_TIME RWTO_TKOFF SDLOG_BOOT_BAT SDLOG_DIRS_MAX SDLOG_MISSION SDLOG_MODE SDLOG_PROFILE SDLOG_UTC_OFFSET SDLOG_UUID SENS_BARO_QNH SENS_BARO_RATE SENS_EXT_I2C_PRB SENS_FLOW_MAXHGT SENS_FLOW_MAXR SENS_FLOW_MINHGT SENS_FLOW_ROT SENS_IMU_MODE SENS_MAG_MODE SENS_MAG_RATE SER_GPS1_BAUD SER_TEL1_BAUD SER_TEL2_BAUD SER_TEL4_BAUD SYS_BL_UPDATE SYS_CAL_ACCEL SYS_CAL_BARO SYS_CAL_GYRO SYS_FAILURE_EN SYS_HITL SYS_STCK_EN SYS_USE_IO WV_EN WV_GAIN WV_ROLL_MIN WV_YRATE_MAX This device can only utilize a maximum of 1MB flash safely! STM32H7[4|5]xxx STM32F74xxx STM32F76xxx STM32F42x STM32F1xx Low STM32F1xx Med STM32F1xx Hi STM32F1xx XL STM32F1xx Con STM32F??? %s: %llu events %s: %llu events, %lluus elapsed, %.2fus avg, min %lluus max %lluus %5.3fus rms %s: %llu events, %.2fus avg, min %lluus max %lluus %5.3fus rms %s: %llu events %s: %llu events, %lluus elapsed, %.2fus avg, min %lluus max %lluus %5.3fus rms %s: %llu events, %.2f avg, min %lluus max %lluus %5.3fus rms n;^ Qkkbal i]Wb 9a&g MGiI wn>Jj #.zf +o*7 -dibouxXcseEfFgGaAn% dobxXui aAfFeEgG /dev/mmcsd%d part ramtron FM25V01 FM25V01A FM25V02 FM25V02A FM25VN02 FM25V05 FM25VN05 FM25V10 FM25VN10 FM25V20A CY15B104Q MB85RS1MT MB85RS256B /dev/pipe%d uint64_t timestamp;uint32_t armed_time_ms;bool armed;bool prearmed;bool ready_to_arm;bool lockdown;bool manual_lockdown;bool force_failsafe;bool in_esc_calibration_mode;bool soft_stop;uint8_t[4] _padding0; actuator_controls_virtual_mc actuator_controls_virtual_fw actuator_controls_3 actuator_controls_2 actuator_controls uint64_t timestamp;uint64_t timestamp_sample;float[8] control; uint64_t timestamp;uint32_t noutputs;float[16] output;uint8_t[4] _padding0; adc_report uint64_t timestamp;uint32_t device_id;int32_t[12] raw_data;uint32_t resolution;float v_ref;int16_t[12] channel_id;uint8_t[4] _padding0; uint64_t timestamp;float indicated_airspeed_m_s;float true_airspeed_m_s;float air_temperature_celsius;float confidence; uint64_t timestamp;float indicated_airspeed_m_s;float calibrated_airspeed_m_s;float true_airspeed_m_s;float calibrated_ground_minus_wind_m_s;float true_ground_minus_wind_m_s;bool airspeed_sensor_measurement_valid;int8_t selected_airspeed_index;uint8_t[2] _padding0; uint64_t timestamp;float voltage_v;float voltage_filtered_v;float current_a;float current_filtered_a;float average_current_a;float discharged_mah;float remaining;float scale;float temperature;int32_t cell_count;float[10] voltage_cell_v;float max_cell_voltage_delta;uint16_t capacity;uint16_t cycle_count;uint16_t run_time_to_empty;uint16_t average_time_to_empty;uint16_t serial_number;uint16_t manufacture_date;uint16_t state_of_health;uint16_t max_error;uint16_t interface_error;bool connected;uint8_t source;uint8_t priority;uint8_t id;bool is_powering_off;uint8_t warning;uint8_t[4] _padding0; uint64_t timestamp;uint64_t timestamp_utc;double lat;double lon;uint32_t seq;float alt;float ground_distance;float[4] q;int8_t result;uint8_t[3] _padding0; uint64_t timestamp;uint64_t timestamp_utc;uint32_t seq;bool feedback;uint8_t[3] _padding0; uint64_t timestamp;uint16_t status;uint16_t mcc;uint16_t mnc;uint16_t lac;uint8_t failure_reason;uint8_t type;uint8_t quality;uint8_t[5] _padding0; uint64_t timestamp;float[2] original_setpoint;float[2] adapted_setpoint; collision_report uint64_t timestamp;uint32_t id;float time_to_minimum_delta;float altitude_minimum_delta;float horizontal_minimum_delta;uint8_t src;uint8_t action;uint8_t threat_level;uint8_t[5] _padding0; uint64_t timestamp;uint8_t main_state;uint8_t[7] _padding0; uint64_t timestamp;float load;float ram_usage; uint64_t timestamp;uint64_t error_count;float differential_pressure_raw_pa;float differential_pressure_filtered_pa;float temperature;uint32_t device_id; uint64_t timestamp;float min_distance;float max_distance;float current_distance;float variance;float h_fov;float v_fov;float[4] q;int8_t signal_quality;uint8_t type;uint8_t id;uint8_t orientation;uint8_t[4] _padding0; uint64_t timestamp;int16_t airspeed_timestamp_rel;int16_t distance_sensor_timestamp_rel;int16_t optical_flow_timestamp_rel;int16_t vehicle_air_data_timestamp_rel;int16_t vehicle_magnetometer_timestamp_rel;int16_t visual_odometry_timestamp_rel;uint8_t[4] _padding0; uint64_t timestamp;float hpos_drift_rate;float vpos_drift_rate;float hspd;bool blocked;uint8_t[3] _padding0; esc_report uint64_t timestamp;uint32_t esc_errorcount;int32_t esc_rpm;float esc_voltage;float esc_current;uint8_t esc_temperature;uint8_t esc_address;uint8_t esc_state;uint8_t failures;uint8_t[4] _padding0; uint64_t timestamp;uint16_t counter;uint8_t esc_count;uint8_t esc_connectiontype;uint8_t esc_online_flags;uint8_t esc_armed_flags;uint8_t[2] _padding0;esc_report[8] esc; uint64_t timestamp;uint64_t timestamp_sample;float[2] gps_hvel;float gps_vvel;float[2] gps_hpos;float gps_vpos;float[2] ev_hvel;float ev_vvel;float[2] ev_hpos;float ev_vpos;float rng_vpos;float baro_vpos;float[2] aux_hvel;float aux_vvel;float[2] flow;float heading;float[3] mag_field;float[2] drag;float airspeed;float beta;float hagl; uint64_t timestamp;uint64_t timestamp_sample;float[2] vel_body;float[2] vel_ne;float[2] flow_uncompensated_integral;float[2] flow_compensated_integral;float[3] gyro_rate_integral;uint8_t[4] _padding0; uint64_t timestamp;uint64_t last_instance_change;uint32_t instance_changed_count;uint32_t accel_device_id;uint32_t baro_device_id;uint32_t gyro_device_id;uint32_t mag_device_id;float[9] combined_test_ratio;float[9] relative_test_ratio;float[4] accumulated_gyro_error;float[4] accumulated_accel_error;uint8_t primary_instance;uint8_t instances_available;bool[9] healthy;bool gyro_fault_detected;bool accel_fault_detected;uint8_t[7] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t gyro_device_id;float[3] gyro_bias;float[3] gyro_bias_variance;uint32_t accel_device_id;float[3] accel_bias;float[3] accel_bias_variance;uint32_t mag_device_id;float[3] mag_bias;float[3] mag_bias_variance;uint8_t[4] _padding0; uint64_t timestamp;uint64_t timestamp_sample;float[24] states;float[24] covariances;uint8_t n_states;uint8_t[7] _padding0; uint64_t timestamp;uint64_t timestamp_sample;float[3] vibe;float[3] output_tracking_error;uint32_t control_mode_flags;uint32_t filter_fault_flags;float pos_horiz_accuracy;float pos_vert_accuracy;float mag_test_ratio;float vel_test_ratio;float pos_test_ratio;float hgt_test_ratio;float tas_test_ratio;float hagl_test_ratio;float beta_test_ratio;float time_slip;uint32_t accel_device_id;uint32_t gyro_device_id;uint32_t baro_device_id;uint32_t mag_device_id;uint16_t gps_check_fail_flags;uint16_t innovation_check_flags;uint16_t solution_status_flags;bool pre_flt_fail_innov_heading;bool pre_flt_fail_innov_vel_horiz;bool pre_flt_fail_innov_vel_vert;bool pre_flt_fail_innov_height;bool pre_flt_fail_mag_field_disturbed;uint8_t health_flags;uint8_t timeout_flags;uint8_t[3] _padding0; follow_target uint64_t timestamp;double lat;double lon;float alt;float vy;float vx;float vz;uint8_t est_cap;uint8_t[7] _padding0; uint64_t timestamp;uint64_t status;float battery_current;float load_current;float power_generated;float bus_voltage;float bat_current_setpoint;uint32_t runtime;int32_t time_until_maintenance;uint16_t generator_speed;int16_t rectifier_temperature;int16_t generator_temperature;uint8_t[6] _padding0; geofence_result uint64_t timestamp;bool geofence_violated;uint8_t geofence_action;bool home_required;uint8_t[5] _padding0; uint64_t timestamp;uint8_t instance;uint8_t len;uint8_t[79] data;uint8_t[7] _padding0; gps_inject_data uint64_t timestamp;uint8_t len;uint8_t flags;uint8_t[182] data; uint64_t timestamp;double lat;double lon;float alt;float x;float y;float z;float yaw;bool valid_alt;bool valid_hpos;bool valid_lpos;bool manual_home; uint64_t timestamp;uint64_t timestamp_sample;float hover_thrust;float hover_thrust_var;float accel_innov;float accel_innov_var;float accel_innov_test_ratio;float accel_noise_var;bool valid;uint8_t[7] _padding0; uint64_t timestamp;uint64_t timestamp_last_signal;int32_t rssi;uint16_t rc_lost_frame_count;uint16_t rc_total_frame_count;uint16_t rc_ppm_frame_length;uint16_t[18] values;uint8_t channel_count;bool rc_failsafe;bool rc_lost;uint8_t input_source;uint8_t[6] _padding0; iridiumsbd_status uint64_t timestamp;uint64_t last_heartbeat;uint16_t tx_buf_write_index;uint16_t rx_buf_read_index;uint16_t rx_buf_end_index;uint16_t failed_sbd_sessions;uint16_t successful_sbd_sessions;uint16_t num_tx_buf_reset;uint8_t signal_quality;uint8_t state;bool ring_pending;bool tx_buf_write_pending;bool tx_session_pending;bool rx_read_pending;bool rx_session_pending;uint8_t[5] _padding0; irlock_report uint64_t timestamp;float pos_x;float pos_y;float size_x;float size_y;uint16_t signature;uint8_t[6] _padding0; landing_gear uint64_t timestamp;int8_t landing_gear;uint8_t[7] _padding0; landing_target_innovations uint64_t timestamp;float innov_x;float innov_y;float innov_cov_x;float innov_cov_y; landing_target_pose uint64_t timestamp;float x_rel;float y_rel;float z_rel;float vx_rel;float vy_rel;float cov_x_rel;float cov_y_rel;float cov_vx_rel;float cov_vy_rel;float x_abs;float y_abs;float z_abs;bool is_static;bool rel_pos_valid;bool rel_vel_valid;bool abs_pos_valid;uint8_t[4] _padding0; led_control uint64_t timestamp;uint8_t led_mask;uint8_t color;uint8_t mode;uint8_t num_blinks;uint8_t priority;uint8_t[3] _padding0; uint64_t timestamp;uint8_t severity;char[127] text; uint64_t timestamp;float total_written_kb;float write_rate_kb_s;uint32_t dropouts;uint32_t message_gaps;uint32_t buffer_used_bytes;uint32_t buffer_size_bytes;uint8_t type;uint8_t backend;uint8_t num_messages;uint8_t[5] _padding0; uint64_t timestamp;uint64_t timestamp_sample;float x;float y;float z;float r;float flaps;float aux1;float aux2;float aux3;float aux4;float aux5;float aux6;uint8_t data_source;uint8_t[3] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t switch_changes;uint8_t mode_slot;uint8_t arm_switch;uint8_t return_switch;uint8_t loiter_switch;uint8_t offboard_switch;uint8_t kill_switch;uint8_t gear_switch;uint8_t transition_switch;uint8_t mode_switch;uint8_t man_switch;uint8_t acro_switch;uint8_t rattitude_switch;uint8_t stab_switch;uint8_t posctl_switch;uint8_t[6] _padding0; mavlink_log uint64_t timestamp;char[127] text;uint8_t severity; uint64_t timestamp;int32_t current_seq;uint16_t count;uint8_t dataman_id;uint8_t[1] _padding0; uint64_t timestamp;uint32_t instance_count;int32_t seq_reached;uint16_t seq_current;uint16_t seq_total;uint16_t item_changed_index;uint16_t item_do_jump_remaining;bool valid;bool warning;bool finished;bool failure;bool stay_in_failsafe;bool flight_termination;bool item_do_jump_changed;uint8_t execution_mode; mount_orientation uint64_t timestamp;float[3] attitude_euler_angle;uint8_t[4] _padding0; uint64_t timestamp;uint16_t saturation_status;uint8_t[6] _padding0; uint64_t timestamp;uint32_t instance_count;float latitude;float longitude;float time_inside;float acceptance_radius;float loiter_radius;float yaw;float altitude;uint16_t sequence_current;uint16_t nav_cmd;uint8_t frame;uint8_t origin;bool loiter_exit_xtrack;bool force_heading;bool altitude_is_relative;bool autocontinue;bool vtol_back_transition;uint8_t[5] _padding0; obstacle_distance uint64_t timestamp;float increment;float angle_offset;uint16_t[72] distances;uint16_t min_distance;uint16_t max_distance;uint8_t frame;uint8_t sensor_type;uint8_t[2] _padding0; uint64_t timestamp;bool ignore_thrust;bool ignore_attitude;bool ignore_bodyrate_x;bool ignore_bodyrate_y;bool ignore_bodyrate_z;bool ignore_position;bool ignore_velocity;bool ignore_acceleration_force;bool ignore_alt_hold;uint8_t[7] _padding0; uint64_t timestamp;uint32_t uptime;uint32_t ram_usage;uint32_t ram_total;uint32_t[4] storage_type;uint32_t[4] storage_usage;uint32_t[4] storage_total;uint32_t[6] link_type;uint32_t[6] link_tx_rate;uint32_t[6] link_rx_rate;uint32_t[6] link_tx_max;uint32_t[6] link_rx_max;int16_t[4] fan_speed;uint8_t type;uint8_t[8] cpu_cores;uint8_t[10] cpu_combined;uint8_t[4] gpu_cores;uint8_t[10] gpu_combined;int8_t temperature_board;int8_t[8] temperature_core;uint8_t[2] _padding0; uint64_t timestamp;float pixel_flow_x_integral;float pixel_flow_y_integral;float gyro_x_rate_integral;float gyro_y_rate_integral;float gyro_z_rate_integral;float ground_distance_m;uint32_t integration_timespan;uint32_t time_since_last_sonar_update;float max_flow_rate;float min_ground_distance;float max_ground_distance;uint16_t frame_count_since_last_readout;int16_t gyro_temperature;uint8_t sensor_id;uint8_t quality;uint8_t[6] _padding0; orbit_status uint64_t timestamp;double x;double y;float radius;float z;uint8_t frame;uint8_t yaw_behaviour;uint8_t[6] _padding0; parameter_update uint64_t timestamp;uint32_t instance;uint8_t[4] _padding0; uint64_t timestamp;uint64_t ping_time;uint32_t ping_sequence;uint32_t dropped_packets;float rtt_ms;uint8_t system_id;uint8_t component_id;uint8_t[2] _padding0; position_controller_landing_status uint64_t timestamp;float horizontal_slope_displacement;float slope_angle_rad;float flare_length;bool abort_landing;uint8_t[3] _padding0; uint64_t timestamp;float nav_roll;float nav_pitch;float nav_bearing;float target_bearing;float xtrack_error;float wp_dist;float acceptance_radius;float yaw_acceptance;float altitude_acceptance;uint8_t type;uint8_t[3] _padding0; uint64_t timestamp;double lat;double lon;float x;float y;float z;float vx;float vy;float vz;float alt;float yaw;float yawspeed;float loiter_radius;float pitch_min;float a_x;float a_y;float a_z;float acceptance_radius;float cruising_speed;float cruising_throttle;bool valid;uint8_t type;bool position_valid;bool velocity_valid;uint8_t velocity_frame;bool alt_valid;bool yaw_valid;bool yawspeed_valid;int8_t landing_gear;int8_t loiter_direction;bool acceleration_valid;bool acceleration_is_force;bool disable_weather_vane;uint8_t[7] _padding0; uint64_t timestamp;position_setpoint previous;position_setpoint current;position_setpoint next; power_button_state uint64_t timestamp;uint8_t event;uint8_t[7] _padding0; power_monitor uint64_t timestamp;float voltage_v;float current_a;float power_w;int16_t rconf;int16_t rsv;int16_t rbv;int16_t rp;int16_t rc;int16_t rcal;int16_t me;int16_t al;uint8_t[4] _padding0; pwm_input uint64_t timestamp;uint64_t error_count;uint32_t pulse_width;uint32_t period; Not implemented on flash constrained hardware uint64_t timestamp;float voltage_v;float rssi_v;uint16_t free_memory_bytes;int16_t[8] actuators;uint16_t[8] servos;uint16_t[18] raw_inputs;bool status_outputs_armed;bool status_override;bool status_rc_ok;bool status_rc_ppm;bool status_rc_dsm;bool status_rc_sbus;bool status_fmu_ok;bool status_raw_pwm;bool status_mixer_ok;bool status_arm_sync;bool status_init_ok;bool status_failsafe;bool status_safety_off;bool status_fmu_initialized;bool status_rc_st24;bool status_rc_sumd;bool alarm_vbatt_low;bool alarm_temperature;bool alarm_servo_current;bool alarm_acc_current;bool alarm_fmu_lost;bool alarm_rc_lost;bool alarm_pwm_error;bool alarm_vservo_fault;bool arming_io_arm_ok;bool arming_fmu_armed;bool arming_fmu_prearmed;bool arming_manual_override_ok;bool arming_failsafe_custom;bool arming_inair_restart_ok;bool arming_always_pwm_enable;bool arming_rc_handling_disabled;bool arming_lockdown;bool arming_force_failsafe;bool arming_termination_failsafe;bool arming_override_immediate;uint8_t[6] _padding0; qshell_req uint64_t timestamp;uint32_t strlen;uint32_t request_sequence;char[100] cmd;uint8_t[4] _padding0; qshell_retval uint64_t timestamp;int32_t return_value;uint32_t return_sequence; uint64_t timestamp;uint16_t rxerrors;uint16_t fix;uint8_t rssi;uint8_t remote_rssi;uint8_t txbuf;uint8_t noise;uint8_t remote_noise;uint8_t[7] _padding0; uint64_t timestamp;float rollspeed_integ;float pitchspeed_integ;float yawspeed_integ;float additional_integ1; rc_channels uint64_t timestamp;uint64_t timestamp_last_valid;float[18] channels;uint32_t frame_drop_count;uint8_t channel_count;int8_t[27] function;uint8_t rssi;bool signal_lost;uint8_t[6] _padding0; rc_parameter_map uint64_t timestamp;int32_t[3] param_index;float[3] scale;float[3] value0;float[3] value_min;float[3] value_max;bool[3] valid;char[51] param_id;uint8_t[6] _padding0; uint64_t timestamp;float indicated_frequency_rpm;float estimated_accurancy_rpm; uint64_t timestamp;bool safety_switch_available;bool safety_off;bool override_available;bool override_enabled;uint8_t[4] _padding0; uint64_t timestamp;uint8_t count;uint8_t[20] svid;uint8_t[20] used;uint8_t[20] elevation;uint8_t[20] azimuth;uint8_t[20] snr;uint8_t[20] prn;uint8_t[7] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;float x;float y;float z;float temperature;uint32_t error_count;uint8_t[3] clip_counter;uint8_t[5] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;float dt;float scale;int16_t[32] x;int16_t[32] y;int16_t[32] z;uint8_t samples;uint8_t rotation;uint8_t[2] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;uint32_t error_count;float pressure;float temperature; uint64_t timestamp;float[3] gyro_rad;uint32_t gyro_integral_dt;int32_t accelerometer_timestamp_relative;float[3] accelerometer_m_s2;uint32_t accelerometer_integral_dt;uint8_t accelerometer_clipping;uint8_t[3] _padding0; uint64_t timestamp;uint32_t[4] gyro_device_ids;float[3] gyro_offset_0;float[3] gyro_offset_1;float[3] gyro_offset_2;float[3] gyro_offset_3;uint32_t[4] accel_device_ids;float[3] accel_offset_0;float[3] accel_offset_1;float[3] accel_offset_2;float[3] accel_offset_3;uint32_t[4] baro_device_ids;float baro_offset_0;float baro_offset_1;float baro_offset_2;float baro_offset_3; uint64_t timestamp;uint64_t time_utc_usec;int32_t lat;int32_t lon;int32_t alt;int32_t alt_ellipsoid;float s_variance_m_s;float c_variance_rad;float eph;float epv;float hdop;float vdop;int32_t noise_per_ms;int32_t jamming_indicator;float vel_m_s;float vel_n_m_s;float vel_e_m_s;float vel_d_m_s;float cog_rad;int32_t timestamp_time_relative;float heading;float heading_offset;uint8_t fix_type;bool vel_ned_valid;uint8_t satellites_used;uint8_t[5] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;float x;float y;float z;float temperature;uint32_t error_count; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;float dt;float resolution_hz;float[3] peak_frequency;float[4] peak_frequencies_x;float[4] peak_frequencies_y;float[4] peak_frequencies_z; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;float dt;float scale;int16_t[32] x;int16_t[32] y;int16_t[32] z;uint8_t samples;uint8_t rotation;uint8_t[2] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;float x;float y;float z;float temperature;uint32_t error_count;bool is_external;uint8_t[7] _padding0; uint64_t timestamp;float mag_inconsistency_angle;uint8_t[4] _padding0; uint64_t timestamp;uint32_t accel_device_id;uint32_t gyro_device_id; uint64_t timestamp;uint32_t accel_device_id_primary;uint32_t[4] accel_device_ids;float[4] accel_inconsistency_m_s_s;uint32_t gyro_device_id_primary;uint32_t[4] gyro_device_ids;float[4] gyro_inconsistency_rad_s;bool[4] accel_healthy;bool[4] gyro_healthy; uint64_t timestamp;float voltage5v_v;float voltage3v3_v;uint8_t v3v3_valid;uint8_t usb_connected;uint8_t brick_valid;uint8_t usb_valid;uint8_t servo_valid;uint8_t periph_5v_oc;uint8_t hipower_5v_oc;uint8_t[1] _padding0; task_stack_info uint64_t timestamp;uint16_t stack_free;char[24] task_name;uint8_t[6] _padding0; uint64_t timestamp;float altitude_sp;float altitude_filtered;float height_rate_setpoint;float height_rate;float airspeed_sp;float airspeed_filtered;float airspeed_derivative_sp;float airspeed_derivative;float total_energy_error;float energy_distribution_error;float total_energy_rate_error;float energy_distribution_rate_error;float throttle_integ;float pitch_integ;uint8_t mode;uint8_t[7] _padding0; uint64_t timestamp;float data_rate;float rate_multiplier;float rate_rx;float rate_tx;float rate_txerr;uint8_t type;uint8_t mode;bool flow_control;bool forwarding;bool mavlink_v2;bool ftp;uint8_t streams;bool heartbeat_type_antenna_tracker;bool heartbeat_type_gcs;bool heartbeat_type_onboard_controller;bool heartbeat_type_gimbal;bool heartbeat_type_adsb;bool heartbeat_type_camera;bool heartbeat_component_telemetry_radio;bool heartbeat_component_log;bool heartbeat_component_osd;bool heartbeat_component_obstacle_avoidance;bool heartbeat_component_vio;bool heartbeat_component_pairing_manager;bool heartbeat_component_udp_bridge;bool heartbeat_component_uart_bridge;bool avoidance_system_healthy;uint8_t[6] _padding0; uint64_t timestamp;uint32_t motor_number;float value;uint32_t timeout_ms;uint8_t action;uint8_t driver_instance;uint8_t[2] _padding0; timesync uint64_t timestamp;int64_t tc1;int64_t ts1;uint8_t sys_id;uint8_t seq;uint8_t[6] _padding0; timesync_status uint64_t timestamp;uint64_t remote_timestamp;int64_t observed_offset;int64_t estimated_offset;uint32_t round_trip_time;uint8_t[4] _padding0; uint64_t timestamp;float[3] position;float yaw;float delta;uint8_t[4] _padding0; uint64_t timestamp;float[3] position;float[3] velocity;float[3] acceleration;float yaw;float yaw_speed;bool point_valid;uint8_t type;uint8_t[2] _padding0; uint64_t timestamp;double lat;double lon;uint32_t icao_address;float altitude;float heading;float hor_velocity;float ver_velocity;uint16_t flags;uint16_t squawk;uint8_t altitude_type;char[9] callsign;uint8_t emitter_type;uint8_t tslc;uint8_t[18] uas_id;uint8_t[2] _padding0; uint64_t timestamp;uint32_t duration;uint32_t silence;uint16_t frequency;uint8_t tune_id;bool tune_override;uint8_t volume;uint8_t[3] _padding0; uavcan_parameter_request uint64_t timestamp;int64_t int_value;float real_value;int16_t param_index;uint8_t message_type;uint8_t node_id;char[17] param_id;uint8_t param_type;uint8_t[6] _padding0; uavcan_parameter_value uint64_t timestamp;int64_t int_value;float real_value;int16_t param_index;uint16_t param_count;uint8_t node_id;char[17] param_id;uint8_t param_type;uint8_t[5] _padding0; ulog_stream uint64_t timestamp;uint16_t msg_sequence;uint8_t length;uint8_t first_message_offset;uint8_t flags;uint8_t[249] data;uint8_t[2] _padding0; ulog_stream_ack uint64_t timestamp;uint16_t msg_sequence;uint8_t[6] _padding0; uint64_t timestamp;uint64_t timestamp_sample;float[3] xyz;uint8_t[4] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t baro_device_id;float baro_alt_meter;float baro_temp_celcius;float baro_pressure_pa;float rho;uint8_t[4] _padding0; uint64_t timestamp;uint64_t timestamp_sample;float[3] xyz;uint8_t[4] _padding0; vehicle_angular_velocity_groundtruth uint64_t timestamp;uint64_t timestamp_sample;float[3] xyz;uint8_t[4] _padding0; vehicle_vision_attitude vehicle_attitude_groundtruth uint64_t timestamp;uint64_t timestamp_sample;float[4] q;float[4] delta_q_reset;uint8_t quat_reset_counter;uint8_t[7] _padding0; fw_virtual_attitude_setpoint mc_virtual_attitude_setpoint uint64_t timestamp;float roll_body;float pitch_body;float yaw_body;float yaw_sp_move_rate;float[4] q_d;float[3] thrust_body;bool roll_reset_integral;bool pitch_reset_integral;bool yaw_reset_integral;bool fw_control_yaw;uint8_t apply_flaps;uint8_t[7] _padding0; uint64_t timestamp;double param5;double param6;float param1;float param2;float param3;float param4;float param7;uint16_t command;uint8_t target_system;uint8_t target_component;uint8_t source_system;uint8_t source_component;uint8_t confirmation;bool from_external;uint8_t[4] _padding0; vehicle_command_ack uint64_t timestamp;int32_t result_param2;uint16_t command;uint8_t result;bool from_external;uint8_t result_param1;uint8_t target_system;uint8_t target_component;uint8_t[5] _padding0; uint64_t timestamp;float yawspeed;float speed_xy;float speed_up;float speed_down;float tilt;float min_distance_to_ground;float max_distance_to_ground;bool want_takeoff;uint8_t[3] _padding0; uint64_t timestamp;bool flag_armed;bool flag_external_manual_override_ok;bool flag_control_manual_enabled;bool flag_control_auto_enabled;bool flag_control_offboard_enabled;bool flag_control_rates_enabled;bool flag_control_attitude_enabled;bool flag_control_yawrate_override_enabled;bool flag_control_rattitude_enabled;bool flag_control_force_enabled;bool flag_control_acceleration_enabled;bool flag_control_velocity_enabled;bool flag_control_position_enabled;bool flag_control_altitude_enabled;bool flag_control_climb_rate_enabled;bool flag_control_termination_enabled;bool flag_control_fixed_hdg_enabled;uint8_t[7] _padding0; vehicle_global_position_groundtruth uint64_t timestamp;uint64_t timestamp_sample;double lat;double lon;float alt;float alt_ellipsoid;float delta_alt;float eph;float epv;float terrain_alt;uint8_t lat_lon_reset_counter;uint8_t alt_reset_counter;bool terrain_alt_valid;bool dead_reckoning;uint8_t[4] _padding0; uint64_t timestamp;uint64_t time_utc_usec;int32_t lat;int32_t lon;int32_t alt;int32_t alt_ellipsoid;float s_variance_m_s;float c_variance_rad;float eph;float epv;float hdop;float vdop;int32_t noise_per_ms;int32_t jamming_indicator;float vel_m_s;float vel_n_m_s;float vel_e_m_s;float vel_d_m_s;float cog_rad;int32_t timestamp_time_relative;float heading;float heading_offset;uint8_t fix_type;bool vel_ned_valid;uint8_t satellites_used;uint8_t selected;uint8_t[4] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t accel_device_id;uint32_t gyro_device_id;float[3] delta_angle;float[3] delta_velocity;uint16_t delta_angle_dt;uint16_t delta_velocity_dt;uint8_t delta_velocity_clipping;uint8_t calibration_count;uint8_t[2] _padding0; uint64_t timestamp;uint32_t accel_device_id;uint32_t gyro_device_id;uint32_t[3] accel_clipping;uint32_t accel_error_count;uint32_t gyro_error_count;float accel_vibration_metric;float gyro_vibration_metric;float gyro_coning_vibration;float[3] mean_accel;float[3] mean_gyro;float temperature_accel;float temperature_gyro;uint16_t accel_rate_hz;uint16_t gyro_rate_hz;uint8_t[4] _padding0; uint64_t timestamp;float alt_max;bool freefall;bool ground_contact;bool maybe_landed;bool landed;bool in_ground_effect;uint8_t[7] _padding0; vehicle_local_position_groundtruth uint64_t timestamp;uint64_t timestamp_sample;uint64_t ref_timestamp;double ref_lat;double ref_lon;float x;float y;float z;float[2] delta_xy;float delta_z;float vx;float vy;float vz;float z_deriv;float[2] delta_vxy;float delta_vz;float ax;float ay;float az;float heading;float delta_heading;float ref_alt;float dist_bottom;float eph;float epv;float evh;float evv;float vxy_max;float vz_max;float hagl_min;float hagl_max;bool xy_valid;bool z_valid;bool v_xy_valid;bool v_z_valid;uint8_t xy_reset_counter;uint8_t z_reset_counter;uint8_t vxy_reset_counter;uint8_t vz_reset_counter;uint8_t heading_reset_counter;bool xy_global;bool z_global;bool dist_bottom_valid;uint8_t[4] _padding0; uint64_t timestamp;float x;float y;float z;float yaw;float yawspeed;float vx;float vy;float vz;float[3] acceleration;float[3] jerk;float[3] thrust;uint8_t[4] _padding0; uint64_t timestamp;uint64_t timestamp_sample;uint32_t device_id;float[3] magnetometer_ga;uint8_t calibration_count;uint8_t[7] _padding0; estimator_odometry vehicle_odometry uint64_t timestamp;uint64_t timestamp_sample;float x;float y;float z;float[4] q;float[4] q_offset;float[21] pose_covariance;float vx;float vy;float vz;float rollspeed;float pitchspeed;float yawspeed;float[21] velocity_covariance;uint8_t local_frame;uint8_t velocity_frame;uint8_t[2] _padding0; uint64_t timestamp;float roll;float pitch;float yaw;float[3] thrust_body; uint64_t timestamp;double lat;double lon;float alt;float roll_offset;float pitch_offset;float yaw_offset;uint8_t mode;uint8_t[7] _padding0; uint64_t timestamp;uint64_t nav_state_timestamp;uint32_t onboard_control_sensors_present;uint32_t onboard_control_sensors_enabled;uint32_t onboard_control_sensors_health;uint8_t nav_state;uint8_t arming_state;uint8_t hil_state;bool failsafe;uint8_t system_type;uint8_t system_id;uint8_t component_id;uint8_t vehicle_type;bool is_vtol;bool is_vtol_tailsitter;bool vtol_fw_permanent_stab;bool in_transition_mode;bool in_transition_to_fw;bool rc_signal_lost;uint8_t rc_input_mode;bool data_link_lost;uint8_t data_link_lost_counter;bool high_latency_data_link_lost;bool engine_failure;bool mission_failure;uint8_t failure_detector_status;uint8_t latest_arming_reason;uint8_t latest_disarming_reason;uint8_t[5] _padding0; uint64_t timestamp;bool condition_calibration_enabled;bool condition_system_sensors_initialized;bool condition_system_hotplug_timeout;bool condition_system_returned_to_home;bool condition_auto_mission_available;bool condition_global_position_valid;bool condition_home_position_valid;bool condition_local_position_valid;bool condition_local_velocity_valid;bool condition_local_altitude_valid;bool condition_power_input_valid;bool condition_battery_healthy;bool condition_escs_error;bool circuit_breaker_engaged_power_check;bool circuit_breaker_engaged_airspd_check;bool circuit_breaker_engaged_enginefailure_check;bool circuit_breaker_flight_termination_disabled;bool circuit_breaker_engaged_usb_check;bool circuit_breaker_engaged_posfailure_check;bool circuit_breaker_vtol_fw_arming_check;bool offboard_control_signal_found_once;bool offboard_control_signal_lost;bool offboard_control_set_by_command;bool rc_signal_found_once;bool rc_input_blocked;bool rc_calibration_valid;bool vtol_transition_failure;bool usb_connected;bool avoidance_system_required;bool avoidance_system_valid;uint8_t[2] _padding0; vehicle_trajectory_bezier uint64_t timestamp;uint8_t bezier_order;uint8_t[7] _padding0;trajectory_bezier[5] control_points; uint64_t timestamp;uint8_t type;uint8_t[7] _padding0;trajectory_waypoint[5] waypoints; uint64_t timestamp;bool vtol_in_rw_mode;bool vtol_in_trans_mode;bool in_transition_to_fw;bool vtol_transition_failsafe;bool fw_permanent_stab;uint8_t[3] _padding0; wheel_encoders uint64_t timestamp;int64_t encoder_position;int32_t speed;uint32_t pulses_per_rev; uint64_t timestamp;uint64_t timestamp_sample;float windspeed_north;float windspeed_east;float variance_north;float variance_east;float tas_innov;float tas_innov_var;float tas_scale;float beta_innov;float beta_innov_var;uint8_t source;uint8_t[3] _padding0; uint64_t timestamp;uint64_t timestamp_sample;float yaw_composite;float yaw_variance;float[5] yaw;float[5] innov_vn;float[5] innov_ve;float[5] weight; This is not a bootable disk. Please insert a bootable floppy and press any key to try again ...
@mrpollo - per dev call
davids5
commented
3 years ago davids5
commented
3 years ago
Removing the Help on V2 Saves
Strings Left are - @dagar - I thould we have errno set to numbers only, did that change?