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Separate autopilot multirotor from autopilot wing - dummy files for wing (#14108)

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* separate autopilot multirotor from autopilot wing - dummy files for wing

* fix for lisence header for new files

* filling empty PG structures with uint8_t dummy
This commit is contained in:
Ivan Efimov 2024-12-30 15:36:33 -06:00 • committed by GitHub
parent 2a50634f67
commit ef81595f1d
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GPG key ID: B5690EEEBB952194
48 changed files with 1345 additions and 194 deletions
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4
src/main/flight/pid.c
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@ -570,7 +570,7 @@ STATIC_UNIT_TESTED FAST_CODE_NOINLINE float pidLevel(int axis, const pidProfile_
#ifdef USE_GPS_RESCUE
angleTarget += gpsRescueAngle[axis] / 100.0f; // Angle is in centidegrees, stepped on roll at 10Hz but not on pitch
#endif
#ifdef USE_POSITION_HOLD
#if defined(USE_POSITION_HOLD) && !defined(USE_WING)
if (FLIGHT_MODE(POS_HOLD_MODE)) {
angleFeedforward = 0.0f; // otherwise the lag of the PT3 carries recent stick inputs into the hold
if (isAutopilotInControl()) {
@ -1127,7 +1127,7 @@ void FAST_CODE pidController(const pidProfile_t *pidProfile, timeUs_t currentTim
|| FLIGHT_MODE(ALT_HOLD_MODE) // todo - check if this is needed
#endif
#ifdef USE_POSITION_HOLD
|| FLIGHT_MODE(POS_HOLD_MODE)
|| FLIGHT_MODE(POS_HOLD_MODE)
#endif
;
levelMode_e levelMode;