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Merge branch 'corvuscorax/OP-1177_althold_cruisecontrol_cleanups' into rel-14.01
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commit
6ce7907cd3
@ -48,7 +48,6 @@
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#include <math.h>
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#include <pid.h>
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#include <CoordinateConversions.h>
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#include <attitudestate.h>
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#include <altitudeholdsettings.h>
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#include <altitudeholddesired.h> // object that will be updated by the module
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#include <altitudeholdstatus.h>
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@ -170,21 +169,6 @@ static void altitudeHoldTask(void)
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// velocity control loop
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throttle = startThrottle - pid_apply_setpoint(&pid1, 1.0f, altitudeHoldStatus.VelocityDesired, velocityStateDown, 1000.0f / DESIRED_UPDATE_RATE_MS);
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// compensate throttle for current attitude
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// Rbe[2][2] in the rotation matrix is the rotated down component of a
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// 0,0,1 vector
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// it is used to scale the throttle, but only up to 4 times the regular
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// throttle
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AttitudeStateData attitudeState;
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AttitudeStateGet(&attitudeState);
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float Rbe[3][3];
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Quaternion2R(&attitudeState.q1, Rbe);
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if (fabsf(Rbe[2][2]) > 0.25f) {
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throttle /= Rbe[2][2];
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} else {
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throttle /= 0.25f;
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}
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if (throttle >= 1.0f) {
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throttle = 1.0f;
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}
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