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https://github.com/iNavFlight/inav.git
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Disable ALTHOLD on user motor stop request
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parent
99f7b1daf2
commit
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4 changed files with 40 additions and 24 deletions
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@ -38,6 +38,7 @@
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#include "fc/config.h"
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#include "fc/rc_controls.h"
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#include "fc/rc_modes.h"
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#include "fc/runtime_config.h"
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#include "flight/failsafe.h"
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@ -350,17 +351,11 @@ void mixTable(const float dT)
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}
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// Motor stop handling
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if (feature(FEATURE_MOTOR_STOP) && ARMING_FLAG(ARMED)) {
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bool failsafeMotorStop = failsafeRequiresMotorStop();
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bool navMotorStop = !failsafeIsActive() && STATE(NAV_MOTOR_STOP_OR_IDLE);
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bool userMotorStop = !navigationIsFlyingAutonomousMode() && !failsafeIsActive() && (rcData[THROTTLE] < rxConfig()->mincheck);
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if (failsafeMotorStop || navMotorStop || userMotorStop) {
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if (feature(FEATURE_3D)) {
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motor[i] = PWM_RANGE_MIDDLE;
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}
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else {
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motor[i] = motorConfig()->mincommand;
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}
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if (ARMING_FLAG(ARMED) && (getMotorStatus() != MOTOR_RUNNING)) {
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if (feature(FEATURE_MOTOR_STOP)) {
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motor[i] = (feature(FEATURE_3D) ? PWM_RANGE_MIDDLE : motorConfig()->mincommand);
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} else {
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motor[i] = motorConfig()->minthrottle;
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}
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}
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}
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@ -373,3 +368,14 @@ void mixTable(const float dT)
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/* Apply motor acceleration/deceleration limit */
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applyMotorRateLimiting(dT);
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}
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motorStatus_e getMotorStatus(void)
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{
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if (failsafeRequiresMotorStop() || (!failsafeIsActive() && STATE(NAV_MOTOR_STOP_OR_IDLE)))
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return MOTOR_STOPPED_AUTO;
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if ((STATE(FIXED_WING) || !isAirmodeActive()) && (!navigationIsFlyingAutonomousMode()) && (!failsafeIsActive()) && (rcData[THROTTLE] < rxConfig()->mincheck))
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return MOTOR_STOPPED_USER;
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return MOTOR_RUNNING;
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}
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@ -85,12 +85,19 @@ typedef struct motorConfig_s {
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PG_DECLARE(motorConfig_t, motorConfig);
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typedef enum {
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MOTOR_STOPPED_USER,
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MOTOR_STOPPED_AUTO,
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MOTOR_RUNNING
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} motorStatus_e;
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extern int16_t motor[MAX_SUPPORTED_MOTORS];
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extern int16_t motor_disarmed[MAX_SUPPORTED_MOTORS];
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uint8_t getMotorCount(void);
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float getMotorMixRange(void);
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bool mixerIsOutputSaturated(void);
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motorStatus_e getMotorStatus(void);
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void writeAllMotors(int16_t mc);
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void mixerUsePWMIOConfiguration(void);
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@ -41,6 +41,7 @@
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#include "fc/runtime_config.h"
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#include "flight/imu.h"
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#include "flight/mixer.h"
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#include "flight/pid.h"
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#include "io/beeper.h"
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@ -2762,7 +2763,7 @@ rthState_e getStateOfForcedRTH(void)
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bool navigationIsControllingThrottle(void)
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{
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navigationFSMStateFlags_t stateFlags = navGetCurrentStateFlags();
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return (stateFlags & (NAV_CTL_ALT | NAV_CTL_EMERG | NAV_CTL_LAUNCH | NAV_CTL_LAND));
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return ((stateFlags & (NAV_CTL_ALT | NAV_CTL_EMERG | NAV_CTL_LAUNCH | NAV_CTL_LAND)) && (getMotorStatus() != MOTOR_STOPPED_USER));
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}
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bool navigationIsFlyingAutonomousMode(void)
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@ -527,23 +527,25 @@ void applyFixedWingNavigationController(navigationFSMStateFlags_t navStateFlags,
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#ifdef NAV_FW_LIMIT_MIN_FLY_VELOCITY
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// Don't apply anything if ground speed is too low (<3m/s)
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if (posControl.actualState.velXY > 300) {
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if (navStateFlags & NAV_CTL_ALT)
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#else
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if (true) {
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#endif
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if (navStateFlags & NAV_CTL_ALT) {
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if (getMotorStatus() == MOTOR_STOPPED_USER) {
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// Motor has been stopped by user. Update target altitude and bypass navigation pitch/throttle control
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resetFixedWingAltitudeController();
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setDesiredPosition(&navGetCurrentActualPositionAndVelocity()->pos, posControl.actualState.yaw, NAV_POS_UPDATE_Z);
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} else
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applyFixedWingAltitudeAndThrottleController(currentTimeUs);
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}
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if (navStateFlags & NAV_CTL_POS)
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applyFixedWingPositionController(currentTimeUs);
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}
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else {
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} else {
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posControl.rcAdjustment[PITCH] = 0;
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posControl.rcAdjustment[ROLL] = 0;
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}
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#else
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if (navStateFlags & NAV_CTL_ALT)
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applyFixedWingAltitudeAndThrottleController(currentTimeUs);
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if (navStateFlags & NAV_CTL_POS)
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applyFixedWingPositionController(currentTimeUs);
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#endif
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//if (navStateFlags & NAV_CTL_YAW)
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if ((navStateFlags & NAV_CTL_ALT) || (navStateFlags & NAV_CTL_POS))
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