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Make yaw controller configurable

This commit is contained in:
Pawel Spychalski (DzikuVx) 2019-12-26 11:10:53 +01:00
parent 243220ab37
commit 746d7423e8
7 changed files with 56 additions and 11 deletions

View file

@ -210,8 +210,10 @@ void resetFixedWingPositionController(void)
virtualDesiredPosition.z = 0;
navPidReset(&posControl.pids.fw_nav);
navPidReset(&posControl.pids.fw_heading);
posControl.rcAdjustment[ROLL] = 0;
posControl.rcAdjustment[YAW] = 0;
posControl.rcAdjustment[YAW] = 0;
isRollAdjustmentValid = false;
isYawAdjustmentValid = false;
@ -295,7 +297,10 @@ static void updatePositionHeadingController_FW(timeUs_t currentTimeUs, timeDelta
// We have virtual position target, calculate heading error
int32_t virtualTargetBearing = calculateBearingToDestination(&virtualDesiredPosition);
// Calculate NAV heading error
/*
* Calculate NAV heading error
* Units are centidegrees
*/
navHeadingError = wrap_18000(virtualTargetBearing - posControl.actualState.yaw);
// Forced turn direction
@ -341,12 +346,34 @@ static void updatePositionHeadingController_FW(timeUs_t currentTimeUs, timeDelta
* Yaw adjustment
* It is working in relative mode and we aim to keep error at zero
*/
float yawAdjustment = navPidApply2(&posControl.pids.fw_heading, 0, navHeadingError, US2S(deltaMicros),
-500,
500,
pidFlags);
if (navConfig()->fw.useFwNavYawControl) {
posControl.rcAdjustment[YAW] = yawAdjustment;
static float limit = 0.0f;
if (limit == 0.0f) {
limit = pidProfile()->navFwPosHdgPidsumLimit * 100.0f;
}
float yawAdjustment = navPidApply2(
&posControl.pids.fw_heading,
0,
navHeadingError,
US2S(deltaMicros),
-limit,
limit,
pidFlags
) / 100.0f;
DEBUG_SET(DEBUG_NAV_YAW, 0, posControl.pids.fw_heading.proportional);
DEBUG_SET(DEBUG_NAV_YAW, 1, posControl.pids.fw_heading.integral);
DEBUG_SET(DEBUG_NAV_YAW, 2, posControl.pids.fw_heading.derivative);
DEBUG_SET(DEBUG_NAV_YAW, 3, navHeadingError);
DEBUG_SET(DEBUG_NAV_YAW, 4, posControl.pids.fw_heading.output_constrained);
posControl.rcAdjustment[YAW] = yawAdjustment;
} else {
posControl.rcAdjustment[YAW] = 0;
}
}
void applyFixedWingPositionController(timeUs_t currentTimeUs)