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Merge remote-tracking branch 'origin/amorale/OP-999_ah_failsafe' into next
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commit
04326e2386
@ -63,6 +63,7 @@
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#define STACK_SIZE_BYTES 1024
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#define TASK_PRIORITY (tskIDLE_PRIORITY + 1)
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#define ACCEL_DOWNSAMPLE 4
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#define TIMEOUT_TRESHOLD 200000
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// Private types
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// Private variables
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@ -130,7 +131,9 @@ static void altitudeHoldTask(__attribute__((unused)) void *parameters)
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// Force update of the settings
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SettingsUpdatedCb(&ev);
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// Failsafe handling
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uint32_t lastAltitudeHoldDesiredUpdate = 0;
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bool enterFailSafe = false;
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// Listen for updates.
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AltitudeHoldDesiredConnectQueue(queue);
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BaroAltitudeConnectQueue(queue);
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@ -144,6 +147,7 @@ static void altitudeHoldTask(__attribute__((unused)) void *parameters)
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// Main task loop
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bool baro_updated = false;
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while (1) {
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enterFailSafe = PIOS_DELAY_DiffuS(lastAltitudeHoldDesiredUpdate) > TIMEOUT_TRESHOLD;
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// Wait until the AttitudeRaw object is updated, if a timeout then go to failsafe
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if (xQueueReceive(queue, &ev, 100 / portTICK_RATE_MS) != pdTRUE) {
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if (!running) {
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@ -173,6 +177,7 @@ static void altitudeHoldTask(__attribute__((unused)) void *parameters)
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starting_altitude = altHold.Altitude;
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} else if (flightStatus.FlightMode != FLIGHTSTATUS_FLIGHTMODE_ALTITUDEHOLD) {
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running = false;
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lastAltitudeHoldDesiredUpdate = PIOS_DELAY_GetRaw();
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}
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} else if (ev.obj == AccelsHandle()) {
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static uint32_t timeval;
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@ -352,6 +357,7 @@ static void altitudeHoldTask(__attribute__((unused)) void *parameters)
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}
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if (!running) {
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lastAltitudeHoldDesiredUpdate = PIOS_DELAY_GetRaw();
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continue;
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}
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@ -370,24 +376,31 @@ static void altitudeHoldTask(__attribute__((unused)) void *parameters)
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// Instead of explicit limit on integral you output limit feedback
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StabilizationDesiredGet(&stabilizationDesired);
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stabilizationDesired.Throttle = error * altitudeHoldSettings.Kp + throttleIntegral -
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altHold.Velocity * altitudeHoldSettings.Kd - altHold.Accel * altitudeHoldSettings.Ka;
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if (stabilizationDesired.Throttle > 1) {
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throttleIntegral -= (stabilizationDesired.Throttle - 1);
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stabilizationDesired.Throttle = 1;
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} else if (stabilizationDesired.Throttle < 0) {
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throttleIntegral -= stabilizationDesired.Throttle;
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stabilizationDesired.Throttle = 0;
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if (!enterFailSafe) {
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stabilizationDesired.Throttle = error * altitudeHoldSettings.Kp + throttleIntegral -
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altHold.Velocity * altitudeHoldSettings.Kd - altHold.Accel * altitudeHoldSettings.Ka;
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if (stabilizationDesired.Throttle > 1) {
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throttleIntegral -= (stabilizationDesired.Throttle - 1);
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stabilizationDesired.Throttle = 1;
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} else if (stabilizationDesired.Throttle < 0) {
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throttleIntegral -= stabilizationDesired.Throttle;
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stabilizationDesired.Throttle = 0;
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}
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} else {
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// shutdown motors
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stabilizationDesired.Throttle = -1;
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}
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stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_ROLL] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
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stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_PITCH] = STABILIZATIONDESIRED_STABILIZATIONMODE_ATTITUDE;
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stabilizationDesired.StabilizationMode[STABILIZATIONDESIRED_STABILIZATIONMODE_YAW] = STABILIZATIONDESIRED_STABILIZATIONMODE_AXISLOCK;
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stabilizationDesired.Roll = altitudeHoldDesired.Roll;
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stabilizationDesired.Pitch = altitudeHoldDesired.Pitch;
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stabilizationDesired.Yaw = altitudeHoldDesired.Yaw;
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StabilizationDesiredSet(&stabilizationDesired);
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} else if (ev.obj == AltitudeHoldDesiredHandle()) {
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// reset the failsafe timer
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lastAltitudeHoldDesiredUpdate = PIOS_DELAY_GetRaw();
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AltitudeHoldDesiredGet(&altitudeHoldDesired);
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}
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}
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@ -811,6 +811,11 @@ static void altitudeHoldDesired(ManualControlCommandData *cmd, bool changed)
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const float DEADBAND_HIGH = 1.0f / 2 + DEADBAND / 2;
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const float DEADBAND_LOW = 1.0f / 2 - DEADBAND / 2;
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// Stop updating AltitudeHoldDesired triggering a failsafe condition.
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if (cmd->Throttle < 0) {
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return;
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}
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// this is the max speed in m/s at the extents of throttle
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uint8_t throttleRate;
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uint8_t throttleExp;
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