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Fix missing PID gains updates
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parent
efb65c6f5d
commit
33e79030f4
5 changed files with 28 additions and 21 deletions
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@ -150,6 +150,8 @@ static long cmsx_PidWriteback(const OSD_Entry *self)
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cmsx_WritebackPidFromArray(cmsx_pidPitch, PIDPITCH);
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cmsx_WritebackPidFromArray(cmsx_pidYaw, PIDYAW);
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schedulePidGainsUpdate();
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return 0;
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}
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@ -203,6 +205,8 @@ static long cmsx_menuPidAltMag_onExit(const OSD_Entry *self)
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cmsx_WritebackPidFromArray(cmsx_pidVel, PIDVEL);
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masterConfig.profile[profileIndex].pidProfile.P8[PIDMAG] = cmsx_pidMag[0];
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navigationUsePIDs(&masterConfig.profile[profileIndex].pidProfile);
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return 0;
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}
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@ -251,6 +255,8 @@ static long cmsx_menuPidGpsnav_onExit(const OSD_Entry *self)
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cmsx_WritebackPidFromArray(cmsx_pidPosR, PIDPOSR);
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cmsx_WritebackPidFromArray(cmsx_pidNavR, PIDNAVR);
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navigationUsePIDs(&masterConfig.profile[profileIndex].pidProfile);
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return 0;
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}
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@ -1198,12 +1198,13 @@ static mspResult_e mspFcProcessInCommand(uint8_t cmdMSP, sbuf_t *src)
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break;
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case MSP_SET_PID:
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signalRequiredPIDCoefficientsUpdate();
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for (int i = 0; i < PID_ITEM_COUNT; i++) {
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currentProfile->pidProfile.P8[i] = sbufReadU8(src);
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currentProfile->pidProfile.I8[i] = sbufReadU8(src);
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currentProfile->pidProfile.D8[i] = sbufReadU8(src);
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}
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schedulePidGainsUpdate();
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navigationUsePIDs(¤tProfile->pidProfile);
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break;
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case MSP_SET_MODE_RANGE:
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@ -1269,7 +1270,7 @@ static mspResult_e mspFcProcessInCommand(uint8_t cmdMSP, sbuf_t *src)
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currentControlRateProfile->rcYawExpo8 = sbufReadU8(src);
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}
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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} else {
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return MSP_RESULT_ERROR;
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}
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@ -531,7 +531,7 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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controlRateConfig->rates[FD_PITCH] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_RATE, newValue);
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if (adjustmentFunction == ADJUSTMENT_PITCH_RATE) {
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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}
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// follow though for combined ADJUSTMENT_PITCH_ROLL_RATE
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@ -539,13 +539,13 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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newValue = constrain((int)controlRateConfig->rates[FD_ROLL] + delta, CONTROL_RATE_CONFIG_ROLL_PITCH_RATE_MIN, CONTROL_RATE_CONFIG_ROLL_PITCH_RATE_MAX);
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controlRateConfig->rates[FD_ROLL] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_RATE, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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case ADJUSTMENT_YAW_RATE:
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newValue = constrain((int)controlRateConfig->rates[FD_YAW] + delta, CONTROL_RATE_CONFIG_YAW_RATE_MIN, CONTROL_RATE_CONFIG_YAW_RATE_MAX);
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controlRateConfig->rates[FD_YAW] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_RATE, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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case ADJUSTMENT_PITCH_ROLL_P:
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case ADJUSTMENT_PITCH_P:
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@ -553,7 +553,7 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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pidProfile->P8[PIDPITCH] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_P, newValue);
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if (adjustmentFunction == ADJUSTMENT_PITCH_P) {
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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}
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// follow though for combined ADJUSTMENT_PITCH_ROLL_P
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@ -561,7 +561,7 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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newValue = constrain((int)pidProfile->P8[PIDROLL] + delta, 0, 200); // FIXME magic numbers repeated in serial_cli.c
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pidProfile->P8[PIDROLL] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_P, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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case ADJUSTMENT_PITCH_ROLL_I:
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case ADJUSTMENT_PITCH_I:
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@ -569,7 +569,7 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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pidProfile->I8[PIDPITCH] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_I, newValue);
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if (adjustmentFunction == ADJUSTMENT_PITCH_I) {
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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}
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// follow though for combined ADJUSTMENT_PITCH_ROLL_I
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@ -577,7 +577,7 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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newValue = constrain((int)pidProfile->I8[PIDROLL] + delta, 0, 200); // FIXME magic numbers repeated in serial_cli.c
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pidProfile->I8[PIDROLL] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_I, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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case ADJUSTMENT_PITCH_ROLL_D:
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case ADJUSTMENT_PITCH_D:
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@ -585,7 +585,7 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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pidProfile->D8[PIDPITCH] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_PITCH_D, newValue);
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if (adjustmentFunction == ADJUSTMENT_PITCH_D) {
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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}
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// follow though for combined ADJUSTMENT_PITCH_ROLL_D
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@ -593,25 +593,25 @@ void applyStepAdjustment(controlRateConfig_t *controlRateConfig, uint8_t adjustm
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newValue = constrain((int)pidProfile->D8[PIDROLL] + delta, 0, 200); // FIXME magic numbers repeated in serial_cli.c
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pidProfile->D8[PIDROLL] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_ROLL_D, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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case ADJUSTMENT_YAW_P:
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newValue = constrain((int)pidProfile->P8[PIDYAW] + delta, 0, 200); // FIXME magic numbers repeated in serial_cli.c
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pidProfile->P8[PIDYAW] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_P, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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case ADJUSTMENT_YAW_I:
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newValue = constrain((int)pidProfile->I8[PIDYAW] + delta, 0, 200); // FIXME magic numbers repeated in serial_cli.c
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pidProfile->I8[PIDYAW] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_I, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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case ADJUSTMENT_YAW_D:
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newValue = constrain((int)pidProfile->D8[PIDYAW] + delta, 0, 200); // FIXME magic numbers repeated in serial_cli.c
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pidProfile->D8[PIDYAW] = newValue;
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blackboxLogInflightAdjustmentEvent(ADJUSTMENT_YAW_D, newValue);
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signalRequiredPIDCoefficientsUpdate();
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schedulePidGainsUpdate();
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break;
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default:
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break;
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@ -82,7 +82,7 @@ int16_t magHoldTargetHeading;
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static pt1Filter_t magHoldRateFilter;
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// Thrust PID Attenuation factor. 0.0f means fully attenuated, 1.0f no attenuation is applied
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static bool shouldUpdatePIDCoeffs = false;
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static bool pidGainsUpdateRequired = false;
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static float tpaFactor;
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int16_t axisPID[FLIGHT_DYNAMICS_INDEX_COUNT];
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@ -152,9 +152,9 @@ FP-PID has been rescaled to match LuxFloat (and MWRewrite) from Cleanflight 1.13
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#define FP_PID_LEVEL_P_MULTIPLIER 65.6f
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#define FP_PID_YAWHOLD_P_MULTIPLIER 80.0f
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void signalRequiredPIDCoefficientsUpdate(void)
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void schedulePidGainsUpdate(void)
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{
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shouldUpdatePIDCoeffs = true;
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pidGainsUpdateRequired = true;
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}
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void updatePIDCoefficients(const pidProfile_t *pidProfile, const controlRateConfig_t *controlRateConfig, const struct motorConfig_s *motorConfig)
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@ -164,11 +164,11 @@ void updatePIDCoefficients(const pidProfile_t *pidProfile, const controlRateConf
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// Check if throttle changed
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if (rcCommand[THROTTLE] != prevThrottle) {
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prevThrottle = rcCommand[THROTTLE];
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signalRequiredPIDCoefficientsUpdate();
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pidGainsUpdateRequired = true;
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}
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// If nothing changed - don't waste time recalculating coefficients
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if (!shouldUpdatePIDCoeffs) {
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if (!pidGainsUpdateRequired) {
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return;
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}
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@ -235,7 +235,7 @@ void updatePIDCoefficients(const pidProfile_t *pidProfile, const controlRateConf
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}
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}
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shouldUpdatePIDCoeffs = false;
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pidGainsUpdateRequired = false;
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}
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static void pidApplyHeadingLock(const pidProfile_t *pidProfile, pidState_t *pidState)
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@ -87,7 +87,7 @@ struct controlRateConfig_s;
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struct motorConfig_s;
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struct rxConfig_s;
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void signalRequiredPIDCoefficientsUpdate(void);
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void schedulePidGainsUpdate(void);
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void updatePIDCoefficients(const pidProfile_t *pidProfile, const struct controlRateConfig_s *controlRateConfig, const struct motorConfig_s *motorConfig);
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void pidController(const pidProfile_t *pidProfile, const struct controlRateConfig_s *controlRateConfig, const struct rxConfig_s *rxConfig);
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