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Merge pull request #6902 from iNavFlight/dzikuvx-gyro-alpha-beta-gamma
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Alpha-Beta-Gamma filter for gyro
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DzikuVx committed May 1, 2021
2 parents 5a4aaed + b38e19e commit 350345d
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3 changes: 3 additions & 0 deletions docs/Settings.md
Original file line number Diff line number Diff line change
Expand Up @@ -148,6 +148,9 @@
| gps_provider | UBLOX | | | Which GPS protocol to be used, note that UBLOX is 5Hz and UBLOX7 is 10Hz (M8N). |
| gps_sbas_mode | NONE | | | Which SBAS mode to be used |
| gps_ublox_use_galileo | OFF | | | Enable use of Galileo satellites. This is at the expense of other regional constellations, so benefit may also be regional. Requires M8N and Ublox firmware 3.x (or later) [OFF/ON]. |
| gyro_abg_alpha | 0 | 0 | 1 | Alpha factor for Gyro Alpha-Beta-Gamma filter |
| gyro_abg_boost | 0.35 | 0 | 2 | Boost factor for Gyro Alpha-Beta-Gamma filter |
| gyro_abg_half_life | 0.5 | 0 | 10 | Sample half-life for Gyro Alpha-Beta-Gamma filter |
| gyro_dyn_lpf_curve_expo | 5 | 1 | 10 | Expo value for the throttle-to-frequency mapping for Dynamic LPF |
| gyro_dyn_lpf_max_hz | 500 | 40 | 1000 | Maximum frequency of the gyro Dynamic LPF |
| gyro_dyn_lpf_min_hz | 200 | 40 | 400 | Minimum frequency of the gyro Dynamic LPF |
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3 changes: 2 additions & 1 deletion src/main/build/debug.h
Original file line number Diff line number Diff line change
Expand Up @@ -83,6 +83,7 @@ typedef enum {
DEBUG_FW_D,
DEBUG_IMU2,
DEBUG_ALTITUDE,
DEBUG_SMITH_COMPENSATOR,
DEBUG_GYRO_ALPHA_BETA_GAMMA,
DEBUG_SMITH_PREDICTOR,
DEBUG_COUNT
} debugType_e;
66 changes: 66 additions & 0 deletions src/main/common/filter.c
Original file line number Diff line number Diff line change
Expand Up @@ -250,3 +250,69 @@ FAST_CODE void biquadFilterUpdate(biquadFilter_t *filter, float filterFreq, uint
filter->y1 = y1;
filter->y2 = y2;
}

#ifdef USE_ALPHA_BETA_GAMMA_FILTER
void alphaBetaGammaFilterInit(alphaBetaGammaFilter_t *filter, float alpha, float boostGain, float halfLife, float dT) {
// beta, gamma, and eta gains all derived from
// http://yadda.icm.edu.pl/yadda/element/bwmeta1.element.baztech-922ff6cb-e991-417f-93f0-77448f1ef4ec/c/A_Study_Jeong_1_2017.pdf

const float xi = powf(-alpha + 1.0f, 0.25); // fourth rool of -a + 1
filter->xk = 0.0f;
filter->vk = 0.0f;
filter->ak = 0.0f;
filter->jk = 0.0f;
filter->a = alpha;
filter->b = (1.0f / 6.0f) * powf(1.0f - xi, 2) * (11.0f + 14.0f * xi + 11 * xi * xi);
filter->g = 2 * powf(1.0f - xi, 3) * (1 + xi);
filter->e = (1.0f / 6.0f) * powf(1 - xi, 4);
filter->dT = dT;
filter->dT2 = dT * dT;
filter->dT3 = dT * dT * dT;
pt1FilterInit(&filter->boostFilter, 100, dT);

const float boost = boostGain * 100;

filter->boost = (boost * boost / 10000) * 0.003;
filter->halfLife = halfLife != 0 ? powf(0.5f, dT / halfLife): 1.0f;
}

FAST_CODE float alphaBetaGammaFilterApply(alphaBetaGammaFilter_t *filter, float input) {
//xk - current system state (ie: position)
//vk - derivative of system state (ie: velocity)
//ak - derivative of system velociy (ie: acceleration)
//jk - derivative of system acceleration (ie: jerk)
float rk; // residual error

// give the filter limited history
filter->xk *= filter->halfLife;
filter->vk *= filter->halfLife;
filter->ak *= filter->halfLife;
filter->jk *= filter->halfLife;

// update our (estimated) state 'x' from the system (ie pos = pos + vel (last).dT)
filter->xk += filter->dT * filter->vk + (1.0f / 2.0f) * filter->dT2 * filter->ak + (1.0f / 6.0f) * filter->dT3 * filter->jk;

// update (estimated) velocity (also estimated dterm from measurement)
filter->vk += filter->dT * filter->ak + 0.5f * filter->dT2 * filter->jk;
filter->ak += filter->dT * filter->jk;

// what is our residual error (measured - estimated)
rk = input - filter->xk;

// artificially boost the error to increase the response of the filter
rk += pt1FilterApply(&filter->boostFilter, fabsf(rk) * rk * filter->boost);
if ((fabsf(rk * filter->a) > fabsf(input - filter->xk))) {
rk = (input - filter->xk) / filter->a;
}
filter->rk = rk; // for logging

// update our estimates given the residual error.
filter->xk += filter->a * rk;
filter->vk += filter->b / filter->dT * rk;
filter->ak += filter->g / (2.0f * filter->dT2) * rk;
filter->jk += filter->e / (6.0f * filter->dT3) * rk;

return filter->xk;
}

#endif
15 changes: 15 additions & 0 deletions src/main/common/filter.h
Original file line number Diff line number Diff line change
Expand Up @@ -56,6 +56,18 @@ typedef struct firFilter_s {
uint8_t coeffsLength;
} firFilter_t;

typedef struct alphaBetaGammaFilter_s {
float a, b, g, e;
float ak; // derivative of system velociy (ie: acceleration)
float vk; // derivative of system state (ie: velocity)
float xk; // current system state (ie: position)
float jk; // derivative of system acceleration (ie: jerk)
float rk; // residual error
float dT, dT2, dT3;
float halfLife, boost;
pt1Filter_t boostFilter;
} alphaBetaGammaFilter_t;

typedef float (*filterApplyFnPtr)(void *filter, float input);
typedef float (*filterApply4FnPtr)(void *filter, float input, float f_cut, float dt);

Expand Down Expand Up @@ -86,3 +98,6 @@ float biquadFilterReset(biquadFilter_t *filter, float value);
float biquadFilterApplyDF1(biquadFilter_t *filter, float input);
float filterGetNotchQ(float centerFrequencyHz, float cutoffFrequencyHz);
void biquadFilterUpdate(biquadFilter_t *filter, float filterFreq, uint32_t refreshRate, float Q, biquadFilterType_e filterType);

void alphaBetaGammaFilterInit(alphaBetaGammaFilter_t *filter, float alpha, float boostGain, float halfLife, float dT);
float alphaBetaGammaFilterApply(alphaBetaGammaFilter_t *filter, float input);
23 changes: 22 additions & 1 deletion src/main/fc/settings.yaml
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Expand Up @@ -94,7 +94,7 @@ tables:
"VIBE", "CRUISE", "REM_FLIGHT_TIME", "SMARTAUDIO", "ACC",
"ERPM", "RPM_FILTER", "RPM_FREQ", "NAV_YAW", "DYNAMIC_FILTER", "DYNAMIC_FILTER_FREQUENCY",
"IRLOCK", "CD", "KALMAN_GAIN", "PID_MEASUREMENT", "SPM_CELLS", "SPM_VS600", "SPM_VARIO", "PCF8574", "DYN_GYRO_LPF", "FW_D", "IMU2", "ALTITUDE",
"SMITH_COMPENSATOR"]
"GYRO_ALPHA_BETA_GAMMA", "SMITH_PREDICTOR"]
- name: async_mode
values: ["NONE", "GYRO", "ALL"]
- name: aux_operator
Expand Down Expand Up @@ -296,6 +296,27 @@ groups:
min: 0
max: 1
default_value: 0
- name: gyro_abg_alpha
description: "Alpha factor for Gyro Alpha-Beta-Gamma filter"
default_value: 0
field: alphaBetaGammaAlpha
condition: USE_ALPHA_BETA_GAMMA_FILTER
min: 0
max: 1
- name: gyro_abg_boost
description: "Boost factor for Gyro Alpha-Beta-Gamma filter"
default_value: 0.35
field: alphaBetaGammaBoost
condition: USE_ALPHA_BETA_GAMMA_FILTER
min: 0
max: 2
- name: gyro_abg_half_life
description: "Sample half-life for Gyro Alpha-Beta-Gamma filter"
default_value: 0.5
field: alphaBetaGammaHalfLife
condition: USE_ALPHA_BETA_GAMMA_FILTER
min: 0
max: 10

- name: PG_ADC_CHANNEL_CONFIG
type: adcChannelConfig_t
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4 changes: 2 additions & 2 deletions src/main/flight/pid.c
Original file line number Diff line number Diff line change
Expand Up @@ -1087,9 +1087,9 @@ void FAST_CODE pidController(float dT)
#endif

#ifdef USE_SMITH_PREDICTOR
DEBUG_SET(DEBUG_SMITH_COMPENSATOR, axis, pidState[axis].gyroRate);
DEBUG_SET(DEBUG_SMITH_PREDICTOR, axis, pidState[axis].gyroRate);
pidState[axis].gyroRate = applySmithPredictor(axis, &pidState[axis].smithPredictor, pidState[axis].gyroRate);
DEBUG_SET(DEBUG_SMITH_COMPENSATOR, axis + 3, pidState[axis].gyroRate);
DEBUG_SET(DEBUG_SMITH_PREDICTOR, axis + 3, pidState[axis].gyroRate);
#endif

DEBUG_SET(DEBUG_PID_MEASUREMENT, axis, pidState[axis].gyroRate);
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38 changes: 37 additions & 1 deletion src/main/sensors/gyro.c
Original file line number Diff line number Diff line change
Expand Up @@ -104,7 +104,14 @@ EXTENDED_FASTRAM dynamicGyroNotchState_t dynamicGyroNotchState;

#endif

PG_REGISTER_WITH_RESET_TEMPLATE(gyroConfig_t, gyroConfig, PG_GYRO_CONFIG, 12);
#ifdef USE_ALPHA_BETA_GAMMA_FILTER

STATIC_FASTRAM filterApplyFnPtr abgFilterApplyFn;
STATIC_FASTRAM alphaBetaGammaFilter_t abgFilter[XYZ_AXIS_COUNT];

#endif

PG_REGISTER_WITH_RESET_TEMPLATE(gyroConfig_t, gyroConfig, PG_GYRO_CONFIG, 13);

PG_RESET_TEMPLATE(gyroConfig_t, gyroConfig,
.gyro_lpf = SETTING_GYRO_HARDWARE_LPF_DEFAULT,
Expand All @@ -130,6 +137,11 @@ PG_RESET_TEMPLATE(gyroConfig_t, gyroConfig,
.dynamicGyroNotchMinHz = SETTING_DYNAMIC_GYRO_NOTCH_MIN_HZ_DEFAULT,
.dynamicGyroNotchEnabled = SETTING_DYNAMIC_GYRO_NOTCH_ENABLED_DEFAULT,
#endif
#ifdef USE_ALPHA_BETA_GAMMA_FILTER
.alphaBetaGammaAlpha = SETTING_GYRO_ABG_ALPHA_DEFAULT,
.alphaBetaGammaBoost = SETTING_GYRO_ABG_BOOST_DEFAULT,
.alphaBetaGammaHalfLife = SETTING_GYRO_ABG_HALF_LIFE_DEFAULT,
#endif
);

STATIC_UNIT_TESTED gyroSensor_e gyroDetect(gyroDev_t *dev, gyroSensor_e gyroHardware)
Expand Down Expand Up @@ -284,6 +296,24 @@ static void gyroInitFilters(void)
biquadFilterInitNotch(notchFilter1[axis], getLooptime(), gyroConfig()->gyro_notch_hz, gyroConfig()->gyro_notch_cutoff);
}
}

#ifdef USE_ALPHA_BETA_GAMMA_FILTER

abgFilterApplyFn = (filterApplyFnPtr)nullFilterApply;

if (gyroConfig()->alphaBetaGammaAlpha > 0) {
abgFilterApplyFn = (filterApplyFnPtr)alphaBetaGammaFilterApply;
for (int axis = 0; axis < 3; axis++) {
alphaBetaGammaFilterInit(
&abgFilter[axis],
gyroConfig()->alphaBetaGammaAlpha,
gyroConfig()->alphaBetaGammaBoost,
gyroConfig()->alphaBetaGammaHalfLife,
getLooptime() * 1e-6f
);
}
}
#endif
}

bool gyroInit(void)
Expand Down Expand Up @@ -458,6 +488,12 @@ void FAST_CODE NOINLINE gyroUpdate()
gyroADCf = gyroLpfApplyFn((filter_t *) &gyroLpfState[axis], gyroADCf);
gyroADCf = notchFilter1ApplyFn(notchFilter1[axis], gyroADCf);

#ifdef USE_ALPHA_BETA_GAMMA_FILTER
DEBUG_SET(DEBUG_GYRO_ALPHA_BETA_GAMMA, axis, gyroADCf);
gyroADCf = abgFilterApplyFn(&abgFilter[axis], gyroADCf);
DEBUG_SET(DEBUG_GYRO_ALPHA_BETA_GAMMA, axis + 3, gyroADCf);
#endif

#ifdef USE_DYNAMIC_FILTERS
if (dynamicGyroNotchState.enabled) {
gyroDataAnalysePush(&gyroAnalyseState, axis, gyroADCf);
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5 changes: 5 additions & 0 deletions src/main/sensors/gyro.h
Original file line number Diff line number Diff line change
Expand Up @@ -82,6 +82,11 @@ typedef struct gyroConfig_s {
uint16_t dynamicGyroNotchMinHz;
uint8_t dynamicGyroNotchEnabled;
#endif
#ifdef USE_ALPHA_BETA_GAMMA_FILTER
float alphaBetaGammaAlpha;
float alphaBetaGammaBoost;
float alphaBetaGammaHalfLife;
#endif
} gyroConfig_t;

PG_DECLARE(gyroConfig_t, gyroConfig);
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1 change: 1 addition & 0 deletions src/main/target/common.h
Original file line number Diff line number Diff line change
Expand Up @@ -84,6 +84,7 @@
#define USE_PITOT_ADC
#define USE_PITOT_VIRTUAL

#define USE_ALPHA_BETA_GAMMA_FILTER
#define USE_DYNAMIC_FILTERS
#define USE_GYRO_KALMAN
#define USE_SMITH_PREDICTOR
Expand Down

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