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Landing improvements only on targets with enought flash size
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2 changed files with 7 additions and 0 deletions
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@ -408,6 +408,7 @@ void applyFixedWingPitchRollThrottleController(navigationFSMStateFlags_t navStat
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pitchCorrection += posControl.rcAdjustment[PITCH];
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throttleCorrection += DECIDEGREES_TO_DEGREES(pitchCorrection) * navConfig()->fw.pitch_to_throttle;
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#ifdef FIXED_WING_LANDING
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if (navStateFlags & NAV_CTL_LAND) {
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/*
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* During LAND we do not allow to raise THROTTLE when nose is up
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@ -415,8 +416,11 @@ void applyFixedWingPitchRollThrottleController(navigationFSMStateFlags_t navStat
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*/
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throttleCorrection = constrain(throttleCorrection, minThrottleCorrection, 0);
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} else {
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#endif
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throttleCorrection = constrain(throttleCorrection, minThrottleCorrection, maxThrottleCorrection);
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#ifdef FIXED_WING_LANDING
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}
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#endif
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}
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// Speed controller - only apply in POS mode when NOT NAV_CTL_LAND
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@ -443,6 +447,7 @@ void applyFixedWingPitchRollThrottleController(navigationFSMStateFlags_t navStat
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rcCommand[THROTTLE] = constrain(correctedThrottleValue, motorConfig()->minthrottle, motorConfig()->maxthrottle);
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}
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#ifdef FIXED_WING_LANDING
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/*
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* Then altitude is below landing slowdown min. altitude, enable final approach procedure
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* TODO refactor conditions in this metod if logic is proven to be correct
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@ -465,6 +470,7 @@ void applyFixedWingPitchRollThrottleController(navigationFSMStateFlags_t navStat
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*/
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rcCommand[PITCH] = pidAngleToRcCommand(DEGREES_TO_DECIDEGREES(2), pidProfile()->max_angle_inclination[FD_PITCH]);
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}
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#endif
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}
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/*-----------------------------------------------------------
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@ -49,6 +49,7 @@
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#endif
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#if (FLASH_SIZE > 128)
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#define FIXED_WING_LANDING
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#define AUTOTUNE_FIXED_WING
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#define ASYNC_GYRO_PROCESSING
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#define BOOTLOG
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