Open Benjozork opened 3 years ago
Pre-empting the noise that will be created as a result of this issue, this will be locked for contributors only so that we can use this for its intended purpose of tracking.
Looks like I'll need to revert to level deceleration segments / targeted deceleration segments in the case where the available gradient is less than -3deg for the first version.
Working on the reversion logic right now. DECEL plotting somewhat realistically with the test values.
Ok calculating flap 1 and 2 CDA pseudo wpts right now (in-non CDA mode, but this is useful for debugging), and they are too far out at some elevated airfields.
It looks like with higher T/D ratios we are reaching low deceleration rates (observed: -0.11kn/s) causing very long config change CONSTANT_SLOPE segments.
Either
- I really need to add iterative step prediction
- I need to revert to LEVEL_DECELERATION or CONSTANT_DECELERATION below a certain deceleration rate
Done
Aircraft Version
Experimental
Description
Discord Username (optional)
someperson#4953