Open mbuzdalov opened 13 hours ago
Issue details
In my 2" whoop-sized quad, running AutoTune produces nice enough rate and angle PIDs, but too small maximum accelerations.
Example: ATC_ANG_RLL_P of 25+, but ATC_ACCEL_R_MAX of around 1000, written as 4000 because it was clamped from below.
ATC_ANG_RLL_P
ATC_ACCEL_R_MAX
These values are not safe to fly.
Version
GitHub master, commit 3ed6ada2e316c52ee9ebae4202c99c681e891693.
Platform [ ] All [ ] AntennaTracker [X ] Copter [ ] Plane [ ] Rover [ ] Submarine
Airframe type
Quadcopter.
Hardware type
FlywooF405S-AIO
Logs
Two logs are attached, for roll and yaw. They are filtered to 5Hz because the flash chip is very small, but should likely be enough for analysis.
24-12-03_22-19-27_roll.bin.gz 24-12-03_22-56-20_yaw.bin.gz
This is reproducible in SITL, on 4.5 ATC_ACCEL_(R|P)_MAX are around 500k but on master they are 20k.
ATC_ACCEL_(R|P)_MAX
Bug report
Issue details
In my 2" whoop-sized quad, running AutoTune produces nice enough rate and angle PIDs, but too small maximum accelerations.
Example:
ATC_ANG_RLL_P
of 25+, butATC_ACCEL_R_MAX
of around 1000, written as 4000 because it was clamped from below.These values are not safe to fly.
Version
GitHub master, commit 3ed6ada2e316c52ee9ebae4202c99c681e891693.
Platform [ ] All [ ] AntennaTracker [X ] Copter [ ] Plane [ ] Rover [ ] Submarine
Airframe type
Quadcopter.
Hardware type
FlywooF405S-AIO
Logs
Two logs are attached, for roll and yaw. They are filtered to 5Hz because the flash chip is very small, but should likely be enough for analysis.
24-12-03_22-19-27_roll.bin.gz 24-12-03_22-56-20_yaw.bin.gz