remove Absolute Control, update I-Term Rotation

src/main/blackbox/blackbox.c

@@ -1379,9 +1379,6 @@ static bool blackboxWriteSysinfo(void)
         BLACKBOX_PRINT_HEADER_LINE(PARAM_NAME_ANTI_GRAVITY_MODE, "%d",      currentPidProfile->antiGravityMode);
         BLACKBOX_PRINT_HEADER_LINE(PARAM_NAME_ANTI_GRAVITY_THRESHOLD, "%d", currentPidProfile->itermThrottleThreshold);
         BLACKBOX_PRINT_HEADER_LINE(PARAM_NAME_ANTI_GRAVITY_GAIN, "%d",      currentPidProfile->itermAcceleratorGain);
-#ifdef USE_ABSOLUTE_CONTROL
-        BLACKBOX_PRINT_HEADER_LINE(PARAM_NAME_ABS_CONTROL_GAIN, "%d",       currentPidProfile->abs_control_gain);
-#endif
 #ifdef USE_INTEGRATED_YAW_CONTROL
         BLACKBOX_PRINT_HEADER_LINE(PARAM_NAME_USE_INTEGRATED_YAW, "%d",     currentPidProfile->use_integrated_yaw);
 #endif

src/main/cli/settings.c

@@ -1142,13 +1142,6 @@ const clivalue_t valueTable[] = {
     { "horizon_tilt_effect",        VAR_UINT8  | PROFILE_VALUE, .config.minmaxUnsigned = { 0,  250 }, PG_PID_PROFILE, offsetof(pidProfile_t, horizon_tilt_effect) },
     { "horizon_tilt_expert_mode",   VAR_UINT8  | PROFILE_VALUE | MODE_LOOKUP, .config.lookup = { TABLE_OFF_ON }, PG_PID_PROFILE, offsetof(pidProfile_t, horizon_tilt_expert_mode) },
 
-#if defined(USE_ABSOLUTE_CONTROL)
-    { PARAM_NAME_ABS_CONTROL_GAIN,  VAR_UINT8 | PROFILE_VALUE,  .config.minmaxUnsigned = { 0, 20 }, PG_PID_PROFILE, offsetof(pidProfile_t, abs_control_gain) },
-    { "abs_control_limit",          VAR_UINT8 | PROFILE_VALUE,  .config.minmaxUnsigned = { 10, 255 }, PG_PID_PROFILE, offsetof(pidProfile_t, abs_control_limit) },
-    { "abs_control_error_limit",    VAR_UINT8 | PROFILE_VALUE,  .config.minmaxUnsigned = { 1, 45 }, PG_PID_PROFILE, offsetof(pidProfile_t, abs_control_error_limit) },
-    { "abs_control_cutoff",         VAR_UINT8 | PROFILE_VALUE,  .config.minmaxUnsigned = { 1, 45 }, PG_PID_PROFILE, offsetof(pidProfile_t, abs_control_cutoff) },
-#endif
-
 #ifdef USE_INTEGRATED_YAW_CONTROL
     { PARAM_NAME_USE_INTEGRATED_YAW, VAR_UINT8  | PROFILE_VALUE | MODE_LOOKUP, .config.lookup = {TABLE_OFF_ON }, PG_PID_PROFILE, offsetof(pidProfile_t, use_integrated_yaw) },
     { "integrated_yaw_relax",        VAR_UINT8  | PROFILE_VALUE, .config.minmaxUnsigned = { 0, 255 }, PG_PID_PROFILE, offsetof(pidProfile_t, integrated_yaw_relax) },

src/main/flight/pid.c

@@ -78,10 +78,6 @@ FAST_DATA_ZERO_INIT uint32_t targetPidLooptime;
 FAST_DATA_ZERO_INIT pidAxisData_t pidData[XYZ_AXIS_COUNT];
 FAST_DATA_ZERO_INIT pidRuntime_t pidRuntime;
 
-#if defined(USE_ABSOLUTE_CONTROL)
-STATIC_UNIT_TESTED FAST_DATA_ZERO_INIT float axisError[XYZ_AXIS_COUNT];
-#endif
-
 #if defined(USE_THROTTLE_BOOST)
 FAST_DATA_ZERO_INIT float throttleBoost;
 pt1Filter_t throttleLpf;
@@ -160,18 +156,14 @@ void resetPidProfile(pidProfile_t *pidProfile)
         .itermLimit = 400,
         .throttle_boost = 5,
         .throttle_boost_cutoff = 15,
-        .iterm_rotation = false,
+        .iterm_rotation = true,
         .iterm_relax = ITERM_RELAX_RP,
         .iterm_relax_cutoff = ITERM_RELAX_CUTOFF_DEFAULT,
         .iterm_relax_type = ITERM_RELAX_SETPOINT,
         .acro_trainer_angle_limit = 20,
         .acro_trainer_lookahead_ms = 50,
         .acro_trainer_debug_axis = FD_ROLL,
         .acro_trainer_gain = 75,
-        .abs_control_gain = 0,
-        .abs_control_limit = 90,
-        .abs_control_error_limit = 20,
-        .abs_control_cutoff = 11,
         .antiGravityMode = ANTI_GRAVITY_SMOOTH,
         .dterm_lpf1_static_hz = DTERM_LPF1_DYN_MIN_HZ_DEFAULT,
             // NOTE: dynamic lpf is enabled by default so this setting is actually
@@ -285,9 +277,6 @@ void pidResetIterm(void)
 {
     for (int axis = 0; axis < 3; axis++) {
         pidData[axis].I = 0.0f;
-#if defined(USE_ABSOLUTE_CONTROL)
-        axisError[axis] = 0.0f;
-#endif
     }
 }
 
@@ -614,47 +603,29 @@ static float accelerationLimit(int axis, float currentPidSetpoint)
     return currentPidSetpoint;
 }
 
-static void rotateVector(float v[XYZ_AXIS_COUNT], float rotation[XYZ_AXIS_COUNT])
+#define SIN2(R) ((R)-(R)*(R)*(R)/6)
+#define COS2(R) (1.0f-(R)*(R)/2)
+
+static inline void rotateAroundYaw(float *x, float *y, float r)
 {
-    // rotate v around rotation vector rotation
-    // rotation in radians, all elements must be small
-    for (int i = 0; i < XYZ_AXIS_COUNT; i++) {
-        int i_1 = (i + 1) % 3;
-        int i_2 = (i + 2) % 3;
-        float newV = v[i_1] + v[i_2] * rotation[i];
-        v[i_2] -= v[i_1] * rotation[i];
-        v[i_1] = newV;
-    }
+    float a,b,s,c;
+
+    s = SIN2(r);
+    c = COS2(r);
+
+    a = x[0]*c + y[0]*s;
+    b = y[0]*c - x[0]*s;
+
+    x[0] = a;
+    y[0] = b;
 }
 
-STATIC_UNIT_TESTED void rotateItermAndAxisError()
+STATIC_UNIT_TESTED void rotateIterm()
 {
-    if (pidRuntime.itermRotation
-#if defined(USE_ABSOLUTE_CONTROL)
-        || pidRuntime.acGain > 0 || debugMode == DEBUG_AC_ERROR
-#endif
-        ) {
-        const float gyroToAngle = pidRuntime.dT * RAD;
-        float rotationRads[XYZ_AXIS_COUNT];
-        for (int i = FD_ROLL; i <= FD_YAW; i++) {
-            rotationRads[i] = gyro.gyroADCf[i] * gyroToAngle;
-        }
-#if defined(USE_ABSOLUTE_CONTROL)
-        if (pidRuntime.acGain > 0 || debugMode == DEBUG_AC_ERROR) {
-            rotateVector(axisError, rotationRads);
-        }
-#endif
-        if (pidRuntime.itermRotation) {
-            float v[XYZ_AXIS_COUNT];
-            for (int i = 0; i < XYZ_AXIS_COUNT; i++) {
-                v[i] = pidData[i].I;
-            }
-            rotateVector(v, rotationRads );
-            for (int i = 0; i < XYZ_AXIS_COUNT; i++) {
-                pidData[i].I = v[i];
-            }
-        }
+    if (pidRuntime.itermRotation) {
+        rotateAroundYaw(&pidData[FD_ROLL].I, &pidData[FD_ROLL].I, gyro.gyroADCf[FD_YAW] * pidRuntime.dT * RAD);
     }
+
 }
 
 #ifdef USE_RC_SMOOTHING_FILTER
@@ -675,46 +646,6 @@ float FAST_CODE applyRcSmoothingFeedforwardFilter(int axis, float pidSetpointDel
 #endif // USE_RC_SMOOTHING_FILTER
 
 #if defined(USE_ITERM_RELAX)
-#if defined(USE_ABSOLUTE_CONTROL)
-STATIC_UNIT_TESTED void applyAbsoluteControl(const int axis, const float gyroRate, float *currentPidSetpoint, float *itermErrorRate)
-{
-    if (pidRuntime.acGain > 0 || debugMode == DEBUG_AC_ERROR) {
-        const float setpointLpf = pt1FilterApply(&pidRuntime.acLpf[axis], *currentPidSetpoint);
-        const float setpointHpf = fabsf(*currentPidSetpoint - setpointLpf);
-        float acErrorRate = 0;
-        const float gmaxac = setpointLpf + 2 * setpointHpf;
-        const float gminac = setpointLpf - 2 * setpointHpf;
-        if (gyroRate >= gminac && gyroRate <= gmaxac) {
-            const float acErrorRate1 = gmaxac - gyroRate;
-            const float acErrorRate2 = gminac - gyroRate;
-            if (acErrorRate1 * axisError[axis] < 0) {
-                acErrorRate = acErrorRate1;
-            } else {
-                acErrorRate = acErrorRate2;
-            }
-            if (fabsf(acErrorRate * pidRuntime.dT) > fabsf(axisError[axis]) ) {
-                acErrorRate = -axisError[axis] * pidRuntime.pidFrequency;
-            }
-        } else {
-            acErrorRate = (gyroRate > gmaxac ? gmaxac : gminac ) - gyroRate;
-        }
-
-        if (isAirmodeActivated()) {
-            axisError[axis] = constrainf(axisError[axis] + acErrorRate * pidRuntime.dT,
-                -pidRuntime.acErrorLimit, pidRuntime.acErrorLimit);
-            const float acCorrection = constrainf(axisError[axis] * pidRuntime.acGain, -pidRuntime.acLimit, pidRuntime.acLimit);
-            *currentPidSetpoint += acCorrection;
-            *itermErrorRate += acCorrection;
-            DEBUG_SET(DEBUG_AC_CORRECTION, axis, lrintf(acCorrection * 10));
-            if (axis == FD_ROLL) {
-                DEBUG_SET(DEBUG_ITERM_RELAX, 3, lrintf(acCorrection * 10));
-            }
-        }
-        DEBUG_SET(DEBUG_AC_ERROR, axis, lrintf(axisError[axis] * 10));
-    }
-}
-#endif
-
 STATIC_UNIT_TESTED void applyItermRelax(const int axis, const float iterm,
     const float gyroRate, float *itermErrorRate, float *currentPidSetpoint)
 {
@@ -742,10 +673,6 @@ STATIC_UNIT_TESTED void applyItermRelax(const int axis, const float iterm,
                 DEBUG_SET(DEBUG_ITERM_RELAX, 2, lrintf(*itermErrorRate));
             }
         }
-
-#if defined(USE_ABSOLUTE_CONTROL)
-        applyAbsoluteControl(axis, gyroRate, currentPidSetpoint, itermErrorRate);
-#endif
     }
 }
 #endif
@@ -926,7 +853,7 @@ void FAST_CODE pidController(const pidProfile_t *pidProfile, timeUs_t currentTim
         gyroRateDterm[axis] = pidRuntime.dtermLowpass2ApplyFn((filter_t *) &pidRuntime.dtermLowpass2[axis], gyroRateDterm[axis]);
     }
 
-    rotateItermAndAxisError();
+    rotateIterm();
 
 #ifdef USE_RPM_FILTER
     rpmFilterUpdate();
@@ -1002,19 +929,13 @@ void FAST_CODE pidController(const pidProfile_t *pidProfile, timeUs_t currentTim
 
         const float previousIterm = pidData[axis].I;
         float itermErrorRate = errorRate;
-#ifdef USE_ABSOLUTE_CONTROL
-        float uncorrectedSetpoint = currentPidSetpoint;
-#endif
 
 #if defined(USE_ITERM_RELAX)
         if (!launchControlActive && !pidRuntime.inCrashRecoveryMode) {
             applyItermRelax(axis, previousIterm, gyroRate, &itermErrorRate, &currentPidSetpoint);
             errorRate = currentPidSetpoint - gyroRate;
         }
 #endif
-#ifdef USE_ABSOLUTE_CONTROL
-        float setpointCorrection = currentPidSetpoint - uncorrectedSetpoint;
-#endif
 
         // --------low-level gyro-based PID based on 2DOF PID controller. ----------
         // 2-DOF PID controller with optional filter on derivative term.
@@ -1114,18 +1035,12 @@ void FAST_CODE pidController(const pidProfile_t *pidProfile, timeUs_t currentTim
         previousGyroRateDterm[axis] = gyroRateDterm[axis];
 
         // -----calculate feedforward component
-#ifdef USE_ABSOLUTE_CONTROL
-        // include abs control correction in feedforward
-        pidSetpointDelta += setpointCorrection - pidRuntime.oldSetpointCorrection[axis];
-        pidRuntime.oldSetpointCorrection[axis] = setpointCorrection;
-#endif
-
         // no feedforward in launch control
         float feedforwardGain = launchControlActive ? 0.0f : pidRuntime.pidCoefficient[axis].Kf;
         if (feedforwardGain > 0) {
             // halve feedforward in Level mode since stick sensitivity is weaker by about half
             feedforwardGain *= FLIGHT_MODE(ANGLE_MODE) ? 0.5f : 1.0f;
-            // transition now calculated in feedforward.c when new RC data arrives 
+            // transition now calculated in feedforward.c when new RC data arrives
             float feedForward = feedforwardGain * pidSetpointDelta * pidRuntime.pidFrequency;
 
 #ifdef USE_FEEDFORWARD

src/main/flight/pid.h

@@ -175,10 +175,6 @@ typedef struct pidProfile_s {
     uint8_t acro_trainer_debug_axis;        // The axis for which record debugging values are captured 0=roll, 1=pitch
     uint8_t acro_trainer_gain;              // The strength of the limiting. Raising may reduce overshoot but also lead to oscillation around the angle limit
     uint16_t acro_trainer_lookahead_ms;     // The lookahead window in milliseconds used to reduce overshoot
-    uint8_t abs_control_gain;               // How strongly should the absolute accumulated error be corrected for
-    uint8_t abs_control_limit;              // Limit to the correction
-    uint8_t abs_control_error_limit;        // Limit to the accumulated error
-    uint8_t abs_control_cutoff;             // Cutoff frequency for path estimation in abs control
     uint8_t dterm_lpf2_type;                // Filter type for 2nd dterm lowpass
     uint16_t dterm_lpf1_dyn_min_hz;         // Dterm lowpass filter 1 min hz when in dynamic mode
     uint16_t dterm_lpf1_dyn_max_hz;         // Dterm lowpass filter 1 max hz when in dynamic mode
@@ -319,15 +315,6 @@ typedef struct pidRuntime_s {
     uint8_t itermRelaxCutoff;
 #endif
 
-#ifdef USE_ABSOLUTE_CONTROL
-    float acCutoff;
-    float acGain;
-    float acLimit;
-    float acErrorLimit;
-    pt1Filter_t acLpf[XYZ_AXIS_COUNT];
-    float oldSetpointCorrection[XYZ_AXIS_COUNT];
-#endif
-
 #ifdef USE_D_MIN
     pt2Filter_t dMinRange[XYZ_AXIS_COUNT];
     pt2Filter_t dMinLowpass[XYZ_AXIS_COUNT];

src/main/flight/pid_init.c

@@ -210,14 +210,6 @@ void pidInitFilters(const pidProfile_t *pidProfile)
     }
 #endif
 
-#if defined(USE_ABSOLUTE_CONTROL)
-    if (pidRuntime.itermRelax) {
-        for (int i = 0; i < XYZ_AXIS_COUNT; i++) {
-            pt1FilterInit(&pidRuntime.acLpf[i], pt1FilterGain(pidRuntime.acCutoff, pidRuntime.dT));
-        }
-    }
-#endif
-
 #if defined(USE_D_MIN)
     // Initialize the filters for all axis even if the d_min[axis] value is 0
     // Otherwise if the pidProfile->d_min_xxx parameters are ever added to
@@ -338,17 +330,6 @@ void pidInitConfig(const pidProfile_t *pidProfile)
     pidRuntime.acroTrainerGain = (float)pidProfile->acro_trainer_gain / 10.0f;
 #endif // USE_ACRO_TRAINER
 
-#if defined(USE_ABSOLUTE_CONTROL)
-    pidRuntime.acGain = (float)pidProfile->abs_control_gain;
-    pidRuntime.acLimit = (float)pidProfile->abs_control_limit;
-    pidRuntime.acErrorLimit = (float)pidProfile->abs_control_error_limit;
-    pidRuntime.acCutoff = (float)pidProfile->abs_control_cutoff;
-    for (int axis = FD_ROLL; axis <= FD_YAW; axis++) {
-        float iCorrection = -pidRuntime.acGain * PTERM_SCALE / ITERM_SCALE * pidRuntime.pidCoefficient[axis].Kp;
-        pidRuntime.pidCoefficient[axis].Ki = MAX(0.0f, pidRuntime.pidCoefficient[axis].Ki + iCorrection);
-    }
-#endif
-
 #ifdef USE_DYN_LPF
     if (pidProfile->dterm_lpf1_dyn_min_hz > 0) {
         switch (pidProfile->dterm_lpf1_type) {
@@ -440,4 +421,3 @@ void pidCopyProfile(uint8_t dstPidProfileIndex, uint8_t srcPidProfileIndex)
         memcpy(pidProfilesMutable(dstPidProfileIndex), pidProfilesMutable(srcPidProfileIndex), sizeof(pidProfile_t));
     }
 }
-

src/main/msp/msp.c

@@ -1462,7 +1462,7 @@ static bool mspProcessOutCommand(int16_t cmdMSP, sbuf_t *dst)
         sbufWriteU16(dst, (uint16_t)constrain(gpsSol.llh.altCm / 100, 0, UINT16_MAX)); // alt changed from 1m to 0.01m per lsb since MSP API 1.39 by RTH. To maintain backwards compatibility compensate to 1m per lsb in MSP again.
         sbufWriteU16(dst, gpsSol.groundSpeed);
         sbufWriteU16(dst, gpsSol.groundCourse);
-        // Added in API version 1.44    
+        // Added in API version 1.44
         sbufWriteU16(dst, gpsSol.hdop);
         break;
 
@@ -1892,11 +1892,7 @@ static bool mspProcessOutCommand(int16_t cmdMSP, sbuf_t *dst)
         sbufWriteU8(dst, 0);
         sbufWriteU8(dst, 0);
 #endif
-#if defined(USE_ABSOLUTE_CONTROL)
-        sbufWriteU8(dst, currentPidProfile->abs_control_gain);
-#else
         sbufWriteU8(dst, 0);
-#endif
 #if defined(USE_THROTTLE_BOOST)
         sbufWriteU8(dst, currentPidProfile->throttle_boost);
 #else
@@ -2988,11 +2984,7 @@ static mspResult_e mspProcessInCommand(mspDescriptor_t srcDesc, int16_t cmdMSP,
             sbufReadU8(src);
             sbufReadU8(src);
 #endif
-#if defined(USE_ABSOLUTE_CONTROL)
-            currentPidProfile->abs_control_gain = sbufReadU8(src);
-#else
             sbufReadU8(src);
-#endif
 #if defined(USE_THROTTLE_BOOST)
             currentPidProfile->throttle_boost = sbufReadU8(src);
 #else

src/main/target/common_post.h

@@ -401,10 +401,6 @@ extern uint8_t __config_end;
 #undef USE_DYN_IDLE
 #endif
 
-#ifndef USE_ITERM_RELAX
-#undef USE_ABSOLUTE_CONTROL
-#endif
-
 #if defined(USE_CUSTOM_DEFAULTS)
 #define USE_CUSTOM_DEFAULTS_ADDRESS
 #endif

src/main/target/common_pre.h

@@ -399,7 +399,6 @@ extern uint8_t _dmaram_end__;
 #define USE_TELEMETRY_MAVLINK
 #define USE_UNCOMMON_MIXERS
 #define USE_SIGNATURE
-#define USE_ABSOLUTE_CONTROL
 #define USE_HOTT_TEXTMODE
 #define USE_LED_STRIP_STATUS_MODE
 #define USE_VARIO

src/test/Makefile

@@ -288,7 +288,7 @@ scheduler_unittest_SRC := \
 		$(USER_DIR)/common/streambuf.c
 
 scheduler_unittest_DEFINES := \
-		USE_OSD= 
+		USE_OSD=
 
 sensor_gyro_unittest_SRC := \
 		$(USER_DIR)/sensors/gyro.c \
@@ -402,7 +402,6 @@ pid_unittest_SRC :=  \
 pid_unittest_DEFINES := \
 		USE_ITERM_RELAX= \
 		USE_RC_SMOOTHING_FILTER= \
-		USE_ABSOLUTE_CONTROL= \
 		USE_LAUNCH_CONTROL= \
 		USE_FEEDFORWARD=