Merge pull request #101 from luggi/althold-flipable
make flipping the quad safe with althold engaged
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commit
ac4835ef67
36
src/imu.c
36
src/imu.c
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@ -391,24 +391,30 @@ int getEstimatedAltitude(void)
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// set vario
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vario = applyDeadband(vel_tmp, 5);
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if (abs(angle[ROLL]) < 800 && abs(angle[PITCH]) < 800) { // only calculate pid if the copters thrust is facing downwards(<80deg)
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// Altitude P-Controller
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error = constrain(AltHold - EstAlt, -500, 500);
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error = applyDeadband(error, 10); // remove small P parametr to reduce noise near zero position
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setVel = constrain((cfg.P8[PIDALT] * error / 128), -300, +300); // limit velocity to +/- 3 m/s
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// Altitude P-Controller
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error = constrain(AltHold - EstAlt, -500, 500);
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error = applyDeadband(error, 10); // remove small P parametr to reduce noise near zero position
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setVel = constrain((cfg.P8[PIDALT] * error / 128), -300, +300); // limit velocity to +/- 3 m/s
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// Velocity PID-Controller
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// P
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error = setVel - vel_tmp;
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BaroPID = constrain((cfg.P8[PIDVEL] * error / 32), -300, +300);
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// Velocity PID-Controller
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// P
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error = setVel - vel_tmp;
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BaroPID = constrain((cfg.P8[PIDVEL] * error / 32), -300, +300);
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// I
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errorAltitudeI += (cfg.I8[PIDVEL] * error) / 8;
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errorAltitudeI = constrain(errorAltitudeI, -(1024 * 200), (1024 * 200));
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BaroPID += errorAltitudeI / 1024; // I in range +/-200
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// I
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errorAltitudeI += (cfg.I8[PIDVEL] * error) / 8;
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errorAltitudeI = constrain(errorAltitudeI, -(1024 * 200), (1024 * 200));
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BaroPID += errorAltitudeI / 1024; // I in range +/-200
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// D
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BaroPID -= constrain(cfg.D8[PIDVEL] * (accZ_tmp + accZ_old) / 64, -150, 150);
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// D
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BaroPID -= constrain(cfg.D8[PIDVEL] * (accZ_tmp + accZ_old) / 64, -150, 150);
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} else {
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BaroPID = 0;
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}
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accZ_old = accZ_tmp;
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return 1;
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5
src/mw.c
5
src/mw.c
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@ -854,7 +854,7 @@ void loop(void)
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AltHold = EstAlt;
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isAltHoldChanged = 0;
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}
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rcCommand[THROTTLE] = initialThrottleHold + BaroPID;
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rcCommand[THROTTLE] = constrain(initialThrottleHold + BaroPID, mcfg.minthrottle + 100, mcfg.maxthrottle);
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}
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} else {
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// slow alt changes for apfags
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@ -869,8 +869,7 @@ void loop(void)
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AltHoldCorr = 0;
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isAltHoldChanged = 0;
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}
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rcCommand[THROTTLE] = initialThrottleHold + BaroPID;
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rcCommand[THROTTLE] = constrain(rcCommand[THROTTLE], mcfg.minthrottle + 150, mcfg.maxthrottle);
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rcCommand[THROTTLE] = constrain(initialThrottleHold + BaroPID, mcfg.minthrottle + 100, mcfg.maxthrottle);
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}
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} else {
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// handle fixedwing-related althold. UNTESTED! and probably wrong
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