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Merge pull request #432 from MJ666/Harakiri_PID
Harakiri PID controller
This commit is contained in:
Dominic Clifton
commit
2c2ef14fa9
3 changed files with 136 additions and 2 deletions
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@ -31,7 +31,7 @@ strength of the correction to be backed off in order to avoid overshooting the t
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## PID controllers
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Cleanflight has 5 built-in PID controllers which each have different flight behavior. Each controller requires
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Cleanflight has 6 built-in PID controllers which each have different flight behavior. Each controller requires
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different PID settings for best performance, so if you tune your craft using one PID controller, those settings will
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likely not work well on any of the other controllers.
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@ -121,3 +121,19 @@ PID Controller 4 is an hybrid version of two MultiWii PID controllers. Roll and
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This PID controller was initialy implemented for testing purposes but is also performing quite well.
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For the ALIENWII32 targets the gyroscale is removed for more yaw authority. This will provide best performance on very small multicopters with brushed motors.
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### PID controller 5, "Harakiri"
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PID Controller 5 is an port of the PID controller from the Harakiri firmware.
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The algorithm is leveraging more floating point math. This PID controller also compensates for different looptimes on roll and pitch. It likely don’t need retuning of the PID values when looptime is changing. Actually there are two settings hardcoded which are configurable via the GUI in Harakiri:
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OLD_YAW 0 // [0/1] 0 = multiwii 2.3 yaw, 1 = older yaw.
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MAIN_CUT_HZ 12.0f // (default 12Hz, Range 1-50Hz)
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The PID controller is flight tested and running well with the default PID settings. If you want do acrobatics start slowly.
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Yaw authority is also quite good.
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@ -506,6 +506,121 @@ static void pidMultiWiiHybrid(pidProfile_t *pidProfile, controlRateConfig_t *con
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#endif
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}
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#define RCconstPI 0.159154943092f // 0.5f / M_PI;
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#define MAIN_CUT_HZ 12.0f // (default 12Hz, Range 1-50Hz)
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#define OLD_YAW 0 // [0/1] 0 = multiwii 2.3 yaw, 1 = older yaw.
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static void pidHarakiri(pidProfile_t *pidProfile, controlRateConfig_t *controlRateConfig, uint16_t max_angle_inclination,
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rollAndPitchTrims_t *angleTrim, rxConfig_t *rxConfig)
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{
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UNUSED(rxConfig);
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float delta, RCfactor, rcCommandAxis, MainDptCut;
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float PTerm = 0, ITerm = 0, DTerm = 0, PTermACC = 0, ITermACC = 0, ITermGYRO = 0, error = 0, prop = 0;
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static float lastGyro[2] = {0, 0}, lastDTerm[2] = {0, 0};
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float tmp0flt;
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int32_t tmp0;
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uint8_t axis;
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float ACCDeltaTimeINS = 0;
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float FLOATcycleTime = 0;
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// MainDptCut = RCconstPI / (float)cfg.maincuthz; // Initialize Cut off frequencies for mainpid D
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MainDptCut = RCconstPI / MAIN_CUT_HZ; // maincuthz (default 12Hz, Range 1-50Hz), hardcoded for now
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FLOATcycleTime = (float)constrain(cycleTime, 1, 100000); // 1us - 100ms
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ACCDeltaTimeINS = FLOATcycleTime * 0.000001f; // ACCDeltaTimeINS is in seconds now
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RCfactor = ACCDeltaTimeINS / (MainDptCut + ACCDeltaTimeINS); // used for pt1 element
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if(FLIGHT_MODE(HORIZON_MODE)) prop = (float)MIN(MAX(ABS(rcCommand[PITCH]), ABS(rcCommand[ROLL])), 450) / 450.0f;
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for (axis = 0; axis < 2; axis++) {
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rcCommandAxis = (float)rcCommand[axis]; // Calculate common values for pid controllers
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if (FLIGHT_MODE(ANGLE_MODE) || FLIGHT_MODE(HORIZON_MODE)) {
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#ifdef GPS
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error = constrain(2.0f * rcCommandAxis + GPS_angle[axis], -((int) max_angle_inclination), +max_angle_inclination) - inclination.raw[axis] + angleTrim->raw[axis];
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#else
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error = constrain(2.0f * rcCommandAxis, -((int) max_angle_inclination), +max_angle_inclination) - inclination.raw[axis] + angleTrim->raw[axis];
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#endif
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#ifdef AUTOTUNE
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if (shouldAutotune()) {
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error = DEGREES_TO_DECIDEGREES(autotune(rcAliasToAngleIndexMap[axis], &inclination, DECIDEGREES_TO_DEGREES(error)));
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}
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#endif
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PTermACC = error * (float)pidProfile->P8[PIDLEVEL] * 0.008f;
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tmp0flt = (float)pidProfile->D8[PIDLEVEL] * 5.0f;
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PTermACC = constrain(PTermACC, -tmp0flt, +tmp0flt);
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errorAngleI[axis] = constrain(errorAngleI[axis] + error * ACCDeltaTimeINS, -30.0f, +30.0f);
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ITermACC = errorAngleI[axis] * (float)pidProfile->I8[PIDLEVEL] * 0.08f;
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}
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if (!FLIGHT_MODE(ANGLE_MODE)) {
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if (ABS((int16_t)gyroData[axis]) > 2560) errorGyroI[axis] = 0.0f;
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else {
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error = (rcCommandAxis * 320.0f / (float)pidProfile->P8[axis]) - gyroData[axis];
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errorGyroI[axis] = constrain(errorGyroI[axis] + error * ACCDeltaTimeINS, -192.0f, +192.0f);
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}
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ITermGYRO = errorGyroI[axis] * (float)pidProfile->I8[axis] * 0.01f;
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if (FLIGHT_MODE(HORIZON_MODE)) {
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PTerm = PTermACC + prop * (rcCommandAxis - PTermACC);
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ITerm = ITermACC + prop * (ITermGYRO - ITermACC);
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}
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else {
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PTerm = rcCommandAxis;
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ITerm = ITermGYRO;
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}
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}
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else {
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PTerm = PTermACC;
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ITerm = ITermACC;
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}
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PTerm -= gyroData[axis] * dynP8[axis] * 0.003f;
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delta = (gyroData[axis] - lastGyro[axis]) / ACCDeltaTimeINS;
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lastGyro[axis] = gyroData[axis];
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lastDTerm[axis] += RCfactor * (delta - lastDTerm[axis]);
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DTerm = lastDTerm[axis] * dynD8[axis] * 0.00007f;
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axisPID[axis] = lrintf(PTerm + ITerm - DTerm); // Round up result.
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#ifdef BLACKBOX
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axisPID_P[axis] = PTerm;
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axisPID_I[axis] = ITerm;
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axisPID_D[axis] = -DTerm;
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#endif
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}
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tmp0flt = (int32_t)FLOATcycleTime & (int32_t)~3; // Filter last 2 bit jitter
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tmp0flt /= 3000.0f;
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if (OLD_YAW) { // [0/1] 0 = multiwii 2.3 yaw, 1 = older yaw. hardcoded for now
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PTerm = ((int32_t)pidProfile->P8[FD_YAW] * (100 - (int32_t)controlRateConfig->yawRate * (int32_t)ABS(rcCommand[FD_YAW]) / 500)) / 100;
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tmp0 = lrintf(gyroData[FD_YAW] * 0.25f);
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PTerm = rcCommand[FD_YAW] - tmp0 * PTerm / 80;
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if ((ABS(tmp0) > 640) || (ABS(rcCommand[FD_YAW]) > 100)) errorGyroI[FD_YAW] = 0;
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else {
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error = ((int32_t)rcCommand[FD_YAW] * 80 / (int32_t)pidProfile->P8[FD_YAW]) - tmp0;
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errorGyroI[FD_YAW] = constrain(errorGyroI[FD_YAW] + (int32_t)(error * tmp0flt), -16000, +16000); // WindUp
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ITerm = (errorGyroI[FD_YAW] / 125 * pidProfile->I8[FD_YAW]) >> 6;
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}
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}
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else {
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tmp0 = ((int32_t)rcCommand[FD_YAW] * (((int32_t)controlRateConfig->yawRate << 1) + 40)) >> 5;
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error = tmp0 - lrintf(gyroData[FD_YAW] * 0.25f); // Less Gyrojitter works actually better
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if (ABS(tmp0) > 50) errorGyroI[FD_YAW] = 0;
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else errorGyroI[FD_YAW] = constrain(errorGyroI[FD_YAW] + (int32_t)(error * (float)pidProfile->I8[FD_YAW] * tmp0flt), -268435454, +268435454);
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ITerm = constrain(errorGyroI[FD_YAW] >> 13, -GYRO_I_MAX, +GYRO_I_MAX);
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PTerm = ((int32_t)error * (int32_t)pidProfile->P8[FD_YAW]) >> 6;
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if(motorCount > 3) { // Constrain FD_YAW by D value if not servo driven in that case servolimits apply
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tmp0 = 300;
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if (pidProfile->D8[FD_YAW]) tmp0 -= (int32_t)pidProfile->D8[FD_YAW];
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PTerm = constrain(PTerm, -tmp0, tmp0);
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}
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}
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axisPID[FD_YAW] = PTerm + ITerm;
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axisPID[FD_YAW] = lrintf(axisPID[FD_YAW]); // Round up result.
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#ifdef BLACKBOX
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axisPID_P[FD_YAW] = PTerm;
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axisPID_I[FD_YAW] = ITerm;
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axisPID_D[FD_YAW] = 0;
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#endif
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}
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static void pidRewrite(pidProfile_t *pidProfile, controlRateConfig_t *controlRateConfig, uint16_t max_angle_inclination,
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rollAndPitchTrims_t *angleTrim, rxConfig_t *rxConfig)
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{
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@ -613,6 +728,9 @@ void setPIDController(int type)
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break;
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case 4:
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pid_controller = pidMultiWiiHybrid;
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break;
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case 5:
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pid_controller = pidHarakiri;
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}
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}
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@ -370,7 +370,7 @@ const clivalue_t valueTable[] = {
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{ "mag_hardware", VAR_UINT8 | MASTER_VALUE, &masterConfig.mag_hardware, 0, MAG_NONE },
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{ "mag_declination", VAR_INT16 | PROFILE_VALUE, &masterConfig.profile[0].mag_declination, -18000, 18000 },
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{ "pid_controller", VAR_UINT8 | PROFILE_VALUE, &masterConfig.profile[0].pidController, 0, 4 },
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{ "pid_controller", VAR_UINT8 | PROFILE_VALUE, &masterConfig.profile[0].pidController, 0, 5 },
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{ "p_pitch", VAR_UINT8 | PROFILE_VALUE, &masterConfig.profile[0].pidProfile.P8[PITCH], 0, 200 },
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{ "i_pitch", VAR_UINT8 | PROFILE_VALUE, &masterConfig.profile[0].pidProfile.I8[PITCH], 0, 200 },
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