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Add landing debug
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parent
9499e78ef8
commit
288015a853
5 changed files with 30 additions and 9 deletions
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@ -612,6 +612,7 @@ bool isFixedWingFlying(void)
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*-----------------------------------------------------------*/
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bool isFixedWingLandingDetected(void)
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{
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DEBUG_SET(DEBUG_LANDING, 4, 0);
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static bool fixAxisCheck = false;
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const bool throttleIsLow = calculateThrottleStatus(THROTTLE_STATUS_TYPE_RC) == THROTTLE_LOW;
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@ -623,6 +624,7 @@ bool isFixedWingLandingDetected(void)
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if (!startCondition || posControl.flags.resetLandingDetector) {
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return fixAxisCheck = posControl.flags.resetLandingDetector = false;
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}
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DEBUG_SET(DEBUG_LANDING, 4, 1);
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static timeMs_t fwLandingTimerStartAt;
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static int16_t fwLandSetRollDatum;
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@ -634,8 +636,12 @@ bool isFixedWingLandingDetected(void)
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bool velCondition = fabsf(navGetCurrentActualPositionAndVelocity()->vel.z) < 50.0f && posControl.actualState.velXY < 100.0f;
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// Check angular rates are low (degs/s)
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bool gyroCondition = averageAbsGyroRates() < 2.0f;
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DEBUG_SET(DEBUG_LANDING, 2, velCondition);
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DEBUG_SET(DEBUG_LANDING, 3, gyroCondition);
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if (velCondition && gyroCondition){
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DEBUG_SET(DEBUG_LANDING, 4, 2);
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DEBUG_SET(DEBUG_LANDING, 5, fixAxisCheck);
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if (!fixAxisCheck) { // capture roll and pitch angles to be used as datums to check for absolute change
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fwLandSetRollDatum = attitude.values.roll; //0.1 deg increments
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fwLandSetPitchDatum = attitude.values.pitch;
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@ -644,6 +650,8 @@ bool isFixedWingLandingDetected(void)
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} else {
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bool isRollAxisStatic = ABS(fwLandSetRollDatum - attitude.values.roll) < 5;
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bool isPitchAxisStatic = ABS(fwLandSetPitchDatum - attitude.values.pitch) < 5;
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DEBUG_SET(DEBUG_LANDING, 6, isRollAxisStatic);
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DEBUG_SET(DEBUG_LANDING, 7, isPitchAxisStatic);
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if (isRollAxisStatic && isPitchAxisStatic) {
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// Probably landed, low horizontal and vertical velocities and no axis rotation in Roll and Pitch
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timeMs_t safetyTimeDelay = 2000 + navConfig()->fw.auto_disarm_delay;
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