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Make use of all 8 debug values for the GPS Rescue debugs (#13055)

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ctzsnooze 2023-08-31 21:58:41 +10:00 • committed by GitHub
parent 7780880139
commit d1025bd1f5
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1 changed files with 25 additions and 9 deletions
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28
src/main/flight/gps_rescue.c
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@ -268,6 +268,7 @@ static void rescueAttainPosition(void)
throttleD *= rescueState.intent.throttleDMultiplier;
// apply user's throttle D gain
throttleD *= gpsRescueConfig()->throttleD;
DEBUG_SET(DEBUG_GPS_RESCUE_THROTTLE_PID, 6, lrintf(throttleD)); // throttle D before lowpass smoothing
// smooth
throttleD = pt2FilterApply(&throttleDLpf, throttleD);
@ -282,8 +283,13 @@ static void rescueAttainPosition(void)
rescueThrottle = gpsRescueConfig()->throttleHover + throttleAdjustment;
rescueThrottle = constrainf(rescueThrottle, gpsRescueConfig()->throttleMin, gpsRescueConfig()->throttleMax);
DEBUG_SET(DEBUG_GPS_RESCUE_THROTTLE_PID, 0, lrintf(throttleP));
DEBUG_SET(DEBUG_GPS_RESCUE_THROTTLE_PID, 1, lrintf(throttleD));
DEBUG_SET(DEBUG_GPS_RESCUE_THROTTLE_PID, 4, lrintf(throttleI));
DEBUG_SET(DEBUG_GPS_RESCUE_THROTTLE_PID, 5, lrintf(tiltAdjustment)); // factor that adjusts throttle based on tilt angle
DEBUG_SET(DEBUG_GPS_RESCUE_THROTTLE_PID, 7, lrintf(throttleAdjustment)); // pidSum; amount to add/subtract from hover throttle value
DEBUG_SET(DEBUG_GPS_RESCUE_TRACKING, 6, lrintf(rescueThrottle)); // throttle value to use during a rescue
/**
Heading / yaw controller
@ -316,6 +322,11 @@ static void rescueAttainPosition(void)
rescueYaw *= GET_DIRECTION(rcControlsConfig()->yaw_control_reversed);
// rescueYaw is the yaw rate in deg/s to correct the heading error
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 5, rollMixAttenuator); // 0-1 to suppress roll adjustments at higher yaw rates
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 6, gpsRescueAngle[AI_ROLL]); // roll added in degrees*100
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 7, rescueYaw); // the yaw rate in deg/s to correct a yaw error
DEBUG_SET(DEBUG_GPS_RESCUE_TRACKING, 7, gpsRescueAngle[AI_ROLL]); // roll added in degrees*100
/**
Pitch / velocity controller
*/
@ -350,7 +361,7 @@ static void rescueAttainPosition(void)
float velocityD = ((velocityError - previousVelocityError) / sampleIntervalNormaliseFactor);
previousVelocityError = velocityError;
velocityD *= gpsRescueConfig()->velD;
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 5, lrintf(velocityD)); // velocity D before lowpass smoothing
// smooth the D steps
const float cutoffHz = rescueState.intent.velocityPidCutoff * rescueState.intent.velocityPidCutoffModifier;
// note that this cutoff is increased up to 2x as we get closer to landing point in descend()
@ -366,6 +377,9 @@ static void rescueAttainPosition(void)
// it gets added to the normal level mode Pitch adjustments in pid.c
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 0, lrintf(velocityP));
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 1, lrintf(velocityD));
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 4, lrintf(velocityI));
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 6, lrintf(rescueState.intent.velocityItermRelax)); // factor attenuates velocity iTerm by multiplication
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 7, lrintf(pitchAdjustment)); // rescue pitch angle in degrees * 100
}
// if initiated too close, and in the climb phase, pitch forward in whatever direction the nose is oriented until min distance away
@ -380,8 +394,8 @@ static void rescueAttainPosition(void)
gpsRescueAngle[AI_PITCH] = pitchAdjustmentFiltered;
// this angle gets added to the normal pitch Angle Mode control values in pid.c - will be seen in pitch setpoint
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 3, lrintf(rescueState.intent.targetVelocityCmS));
DEBUG_SET(DEBUG_GPS_RESCUE_TRACKING, 1, lrintf(rescueState.intent.targetVelocityCmS));
DEBUG_SET(DEBUG_GPS_RESCUE_VELOCITY, 3, lrintf(rescueState.intent.targetVelocityCmS)); // target velocity to home
DEBUG_SET(DEBUG_GPS_RESCUE_TRACKING, 1, lrintf(rescueState.intent.targetVelocityCmS)); // target velocity to home
}
static void performSanityChecks(void)
@ -544,8 +558,7 @@ static void sensorUpdate(void)
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 0, rescueState.sensor.groundSpeedCmS); // groundspeed cm/s
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 1, gpsSol.groundCourse); // degrees * 10
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 2, attitude.values.yaw); // degrees * 10
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 3, rescueState.sensor.directionToHome); // degrees * 10
DEBUG_SET(DEBUG_GPS_RESCUE_HEADING, 3, rescueState.sensor.directionToHome); // computed from current GPS position in relation to home
rescueState.sensor.healthy = gpsIsHealthy();
if (rescueState.phase == RESCUE_LANDING) {
@ -554,7 +567,7 @@ static void sensorUpdate(void)
// Note: subtracting 1G from Z assumes the quad is 'flat' with respect to the horizon. A true non-gravity acceleration value, regardless of attitude, may be better.
}
rescueState.sensor.directionToHome = GPS_directionToHome;
rescueState.sensor.directionToHome = GPS_directionToHome; // extern value from gps.c using current position relative to home
rescueState.sensor.errorAngle = (attitude.values.yaw - rescueState.sensor.directionToHome) / 10.0f;
// both attitude and direction are in degrees * 10, errorAngle is degrees
if (rescueState.sensor.errorAngle <= -180) {
@ -564,6 +577,9 @@ static void sensorUpdate(void)
}
rescueState.sensor.absErrorAngle = fabsf(rescueState.sensor.errorAngle);
DEBUG_SET(DEBUG_GPS_RESCUE_TRACKING, 4, lrintf(attitude.values.yaw)); // estimated heading of the quad (direction nose is pointing in)
DEBUG_SET(DEBUG_GPS_RESCUE_TRACKING, 5, lrintf(rescueState.sensor.directionToHome)); // angle to home derived from GPS location and home position
if (!newGPSData) {
return;
// GPS ground speed, velocity and distance to home will be held at last good values if no new packets