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OP-1483 Added velocity filter to correct EKF's velocity estimate for static velocity offsets

(caused for example by sensor disagreement or calibration issues)
This commit is contained in:
Corvus Corax 2014-09-19 16:34:20 +02:00
parent 1a0ab29050
commit b315c8f106
4 changed files with 155 additions and 1 deletions

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@ -0,0 +1,143 @@
/**
******************************************************************************
* @addtogroup OpenPilotModules OpenPilot Modules
* @{
* @addtogroup State Estimation
* @brief Acquires sensor data and computes state estimate
* @{
*
* @file filtervelocity.c
* @author The OpenPilot Team, http://www.openpilot.org Copyright (C) 2013.
* @brief Barometric altitude filter, calculates altitude offset based on
* GPS altitude offset if available
*
* @see The GNU Public License (GPL) Version 3
*
******************************************************************************/
/*
* This program is free software; you can redistribute it and/or modify
* it under the terms of the GNU General Public License as published by
* the Free Software Foundation; either version 3 of the License, or
* (at your option) any later version.
*
* This program is distributed in the hope that it will be useful, but
* WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY
* or FITNESS FOR A PARTICULAR PURPOSE. See the GNU General Public License
* for more details.
*
* You should have received a copy of the GNU General Public License along
* with this program; if not, write to the Free Software Foundation, Inc.,
* 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
*/
#include "inc/stateestimation.h"
#include <revosettings.h>
// Private constants
#define STACK_REQUIRED 128
#define DT_ALPHA 1e-3f
#define DT_MIN 1e-6f
#define DT_MAX 1.0f
#define DT_INIT (1.0f / 666.0f) // initialize with 666 Hz (default sensor update rate on revo)
// Private types
struct data {
float vel[3];
float velocityBias[3];
float oldPos[3];
float alpha;
uint8_t inited;
PiOSDeltatimeConfig dtconfig;
};
// Private variables
// Private functions
static int32_t init(stateFilter *self);
static filterResult filter(stateFilter *self, stateEstimation *state);
int32_t filterVelocityInitialize(stateFilter *handle)
{
handle->init = &init;
handle->filter = &filter;
handle->localdata = pios_malloc(sizeof(struct data));
return STACK_REQUIRED;
}
static int32_t init(stateFilter *self)
{
struct data *this = (struct data *)self->localdata;
this->vel[0] = 0.0f;
this->vel[1] = 0.0f;
this->vel[2] = 0.0f;
this->velocityBias[0] = 0.0f;
this->velocityBias[1] = 0.0f;
this->velocityBias[2] = 0.0f;
this->oldPos[0] = 0.0f;
this->oldPos[1] = 0.0f;
this->oldPos[2] = 0.0f;
this->inited = 0;
RevoSettingsInitialize();
RevoSettingsVelocityPostProcessingLowPassAlphaGet(&this->alpha);
PIOS_DELTATIME_Init(&this->dtconfig, DT_INIT, DT_MIN, DT_MAX, DT_ALPHA);
return 0;
}
static filterResult filter(stateFilter *self, stateEstimation *state)
{
struct data *this = (struct data *)self->localdata;
if (IS_SET(state->updated, SENSORUPDATES_pos)) {
float dT;
dT = PIOS_DELTATIME_GetAverageSeconds(&this->dtconfig);
// position updates allow us to calculate an ad-hoc velocity estimate
// it will be very noisy and likely quite wrong at every given point in time,
// but its long term average error should be quite low
if (this->inited >= 1) { // only calculate velocity estimate if previous position is known
this->vel[0] = (state->pos[0] - this->oldPos[0]) / dT;
this->vel[1] = (state->pos[1] - this->oldPos[1]) / dT;
this->vel[2] = (state->pos[2] - this->oldPos[2]) / dT;
this->inited = 2;
} else {
// mark previous position as known
this->inited = 1;
}
this->oldPos[0] = state->pos[0];
this->oldPos[1] = state->pos[1];
this->oldPos[2] = state->pos[2];
}
if (IS_SET(state->updated, SENSORUPDATES_vel)) {
// if we have both a velocity estimate from filter and a velocity estimate from postion
// we can calculate a bias estimate. It must be heavily low pass filtered to become useful
// this assumes that the bias is relatively constant over time
if (this->inited >= 2) { // only calculate bias if velocity estimate is calculated
this->velocityBias[0] *= this->alpha;
this->velocityBias[0] += (1.0f - this->alpha) * (this->vel[0] - state->vel[0]);
this->velocityBias[1] *= this->alpha;
this->velocityBias[1] += (1.0f - this->alpha) * (this->vel[1] - state->vel[1]);
this->velocityBias[2] *= this->alpha;
this->velocityBias[2] += (1.0f - this->alpha) * (this->vel[2] - state->vel[2]);
}
state->vel[0] += this->velocityBias[0];
state->vel[1] += this->velocityBias[1];
state->vel[2] += this->velocityBias[2];
}
return FILTERRESULT_OK;
}
/**
* @}
* @}
*/

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@ -77,6 +77,7 @@ typedef struct stateFilterStruct {
int32_t filterMagInitialize(stateFilter *handle);
int32_t filterBaroiInitialize(stateFilter *handle);
int32_t filterBaroInitialize(stateFilter *handle);
int32_t filterVelocityInitialize(stateFilter *handle);
int32_t filterAltitudeInitialize(stateFilter *handle);
int32_t filterAirInitialize(stateFilter *handle);
int32_t filterStationaryInitialize(stateFilter *handle);

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@ -146,6 +146,7 @@ static const filterPipeline *filterChain = NULL;
static stateFilter magFilter;
static stateFilter baroFilter;
static stateFilter baroiFilter;
static stateFilter velocityFilter;
static stateFilter altitudeFilter;
static stateFilter airFilter;
static stateFilter stationaryFilter;
@ -235,7 +236,10 @@ static const filterPipeline *ekf13Queue = &(filterPipeline) {
.filter = &baroFilter,
.next = &(filterPipeline) {
.filter = &ekf13Filter,
.next = NULL,
.next = &(filterPipeline) {
.filter = &velocityFilter,
.next = NULL,
}
}
}
}
@ -298,6 +302,7 @@ int32_t StateEstimationInitialize(void)
stack_required = maxint32_t(stack_required, filterMagInitialize(&magFilter));
stack_required = maxint32_t(stack_required, filterBaroiInitialize(&baroiFilter));
stack_required = maxint32_t(stack_required, filterBaroInitialize(&baroFilter));
stack_required = maxint32_t(stack_required, filterVelocityInitialize(&velocityFilter));
stack_required = maxint32_t(stack_required, filterAltitudeInitialize(&altitudeFilter));
stack_required = maxint32_t(stack_required, filterAirInitialize(&airFilter));
stack_required = maxint32_t(stack_required, filterStationaryInitialize(&stationaryFilter));

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@ -15,6 +15,11 @@
bias = a + b * temp + c * temp^2 + d * temp^3 -->
<field name="BaroTempCorrectionPolynomial" units="" type="float" elements="4" elementnames="a,b,c,d" defaultvalue="0,0,0,0"/>
<field name="BaroTempCorrectionExtent" units="" type="float" elements="2" elementnames="min,max" defaultvalue="0,0"/>
<!-- Coefficient for velocity estimate post processing low pass filter
- filters velocity bias based on delta position to compensate offsets coming from EKF -->
<field name="VelocityPostProcessingLowPassAlpha" units="" type="float" elements="1" defaultvalue="0.9999"/>
<access gcs="readwrite" flight="readwrite"/>
<telemetrygcs acked="true" updatemode="onchange" period="0"/>
<telemetryflight acked="true" updatemode="onchange" period="0"/>