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AHRSEKF.c
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#include "AHRSEKF.h"
#include "stm32f4xx.h"
#include <arm_math.h>
#include "flightConTask.h"
#include "kalman.h"
#include "axisTrans.h"
#include "sensor.h"
xQueueHandle AHRSToFlightConQueue;
xQueueHandle AHRSToINSQueue;
float insBuffer[INS_FRAME_LEN]={0}; //gyr,acc,mag,q,dt
//dt comes last
GFilterType sensorGFT[6]={
{{0},10,9},
{{0},10,9},
{{0},10,9},
{{0},10,9},
{{0},10,9},
{{0},10,9}
};//acc[0],acc[1],acc[2],mag[0],mag[1],mag[2]
float m0[3]={0.0};
float bodyQuat[4]={1,0,0,0}; //姿态四元数
const float P[16]={1, 0, 0, 0,
0, 1, 0, 0,
0, 0, 1, 0,
0, 0, 0, 1};
#ifdef MEASURE_DIM3
const float R[9] = {
100,0,0,
0,100,0,
0,0,100};
#endif
#ifdef MEASURE_DIM6
const float R[36]={
1, 0, 0, 0, 0, 0,
0, 1, 0, 0, 0, 0,
0, 0, 1, 0, 0, 0,
0, 0, 0, 15, 0, 0,
0, 0, 0, 0, 15, 0,
0, 0, 0, 0, 0, 15}; //观测噪声协方差阵
#endif
const float Q[16]={
0.00001, 0, 0, 0,
0, 0.00001, 0, 0,
0, 0, 0.00001,0,
0, 0, 0, 0.00001};
//噪声协方差阵自适应
void SetR(SensorDataType *sdt,float *R,u8 measure_dim)
{
float totalAcc=sqrt(sdt->acc[0]*sdt->acc[0]+sdt->acc[1]*sdt->acc[1]+sdt->acc[2]*sdt->acc[2]);
float gErr=fabs(totalAcc-9.814);
u8 i;
if(gErr<0.4)
{
for(i=0;i<3;i++)
R[i*(measure_dim+1)]=0.2*(1+4/0.4*gErr)+0.8*R[i*(measure_dim+1)];
}
else
{
for(i=0;i<3;i++)
R[i*(measure_dim+1)]=0.2*(5+15/9.814*(gErr-0.4))+0.8*R[i*(measure_dim+1)];
}
}
/*------------------------------tasks----------------------------------------*/
void vAEKFAligTask(void* pvParameters)
{
SensorDataType* pSDT;
SensorDataType sdtBuffer;
portTickType lastReadTime;
float mAngle[3];
float Cbn[9];
u8 i=0,k;
xQueueReceive(xSenToAhrsQueue,&pSDT,portMAX_DELAY);
lastReadTime = xTaskGetTickCount();
for(;;)
{
xQueueReceive(xSenToAhrsQueue,&pSDT,portMAX_DELAY);
sdtBuffer = *pSDT;
//数字滤波
for(k=0;k<3;k++)
{
sdtBuffer.acc[k]=GaussianFilter(&(sensorGFT[k]),sdtBuffer.acc[k]);
sdtBuffer.mag[k]=(s16)(GaussianFilter(&(sensorGFT[k+3]),(float)(sdtBuffer.mag[k])));
}
i++;
vTaskDelayUntil(&lastReadTime,(portTickType)(40/portTICK_RATE_MS));
if(i>50)
{
//calculate normalized geomagnetic
float mag_norm;
MeasureAngle(sdtBuffer.acc,sdtBuffer.mag,mAngle,mAngle,0);
Angle2Quat(bodyQuat,mAngle);
Quat2dcm(Cbn,bodyQuat);
m0[0]=Cbn[0]*sdtBuffer.mag[0]+Cbn[1]*sdtBuffer.mag[1]+Cbn[2]*sdtBuffer.mag[2];
m0[1]=Cbn[3]*sdtBuffer.mag[0]+Cbn[4]*sdtBuffer.mag[1]+Cbn[5]*sdtBuffer.mag[2];
m0[2]=Cbn[6]*sdtBuffer.mag[0]+Cbn[7]*sdtBuffer.mag[1]+Cbn[8]*sdtBuffer.mag[2];
arm_sqrt_f32(m0[0]*m0[0]+m0[1]*m0[1],&(m0[0]));
m0[1]=0.0;
arm_sqrt_f32(m0[0]*m0[0]+m0[2]*m0[2],&mag_norm);
m0[0] /= mag_norm;
m0[2] /= mag_norm;
xTaskCreate(vAEKFProcessTask, (signed portCHAR *)"AHRS_EKF", configMINIMAL_STACK_SIZE+1024, (void *)NULL, tskIDLE_PRIORITY+3,NULL);
vTaskDelete(NULL);
}
}
}
void vAEKFProcessTask(void* pvParameters)
{
u8 i=0;
u8 k;
float dt=0.005;
ekf_filter filter;
#ifdef MEASURE_DIM3
float measure[3]={0};
#endif
#ifdef MEASURE_DIM6
float measure[6]={0};
float Cbn[9]={0.0};
#endif
float angle[3]={0};
portTickType lastTime;
SensorDataType* pSDT;
SensorDataType sdtBuffer;
float *p_insBuffer=insBuffer;
AttConDataType acdt;
filter=ekf_filter_new(4,6,Q,R,AHRS_GetA,AHRS_GetH,AHRS_aFunc,AHRS_hFunc);
memcpy(filter->x,bodyQuat,filter->state_dim*sizeof(float));
memcpy(filter->P,P,filter->state_dim*filter->state_dim*sizeof(float));
xQueueReceive(xSenToAhrsQueue,&pSDT,portMAX_DELAY);
lastTime = xTaskGetTickCount();
for(;;)
{
xQueueReceive(xSenToAhrsQueue,&pSDT,portMAX_DELAY);
sdtBuffer=*pSDT;
acdt.rollAngleRate = sdtBuffer.gyr[0];
acdt.pitchAngleRate = sdtBuffer.gyr[1];
acdt.yawAngleRate = sdtBuffer.gyr[2];
insBuffer[0]=sdtBuffer.acc[0];
insBuffer[1]=sdtBuffer.acc[1];
insBuffer[2]=sdtBuffer.acc[2];
insBuffer[3]=filter->x[0];
insBuffer[4]=filter->x[1];
insBuffer[5]=filter->x[2];
insBuffer[6]=filter->x[3];
insBuffer[INDEX_DT]+=dt;
//数字滤波
for(k=0;k<3;k++)
{
sdtBuffer.acc[k]=GaussianFilter(&(sensorGFT[k]),sdtBuffer.acc[k]);
sdtBuffer.mag[k]=(s16)(GaussianFilter(&(sensorGFT[k+3]),(float)(sdtBuffer.mag[k])));
}
EKF_predict(filter
,(void *)(sdtBuffer.gyr)
,(void *)NULL
,(void *)(&dt)
,(void *)(filter->A)
,(void *)NULL);
if(i++>=10)
{
float norm;
i=0;
//获取观测量
measure[0]=sdtBuffer.acc[0];
measure[1]=sdtBuffer.acc[1];
measure[2]=sdtBuffer.acc[2];
#ifdef MEASURE_DIM6
measure[3]=sdtBuffer.mag[0];
measure[4]=sdtBuffer.mag[1];
measure[5]=sdtBuffer.mag[2];
#endif
//normalize
arm_sqrt_f32(measure[0]*measure[0]+measure[1]*measure[1]+measure[2]*measure[2],&norm);
measure[0] /= norm;
measure[1] /= norm;
measure[2] /= norm;
#ifdef MEASURE_DIM6
arm_sqrt_f32(measure[3]*measure[3]+measure[4]*measure[4]+measure[5]*measure[5],&norm);
measure[3] /= norm;
measure[4] /= norm;
measure[5] /= norm;
#endif
SetR(&sdtBuffer,filter->R,filter->measure_dim);
EKF_update(filter
,measure
,(void *)(filter->x)
,(void *)m0
,(void *)(filter->x)
,(void *)m0);
#ifdef MEASURE_DIM6
//calculate m0, method from paper
Quat2dcm(Cbn,filter->x);
m0[0] = Cbn[0]*measure[3]+Cbn[1]*measure[4]+Cbn[2]*measure[5];
m0[1] = Cbn[3]*measure[3]+Cbn[4]*measure[4]+Cbn[5]*measure[5];
m0[2] = Cbn[6]*measure[3]+Cbn[7]*measure[4]+Cbn[8]*measure[5];
arm_sqrt_f32(m0[0]*m0[0]+m0[1]*m0[1],&(m0[0]));
m0[1]=0.0;
#endif
}
QuatNormalize(filter->x);
Quat2Angle(angle,filter->x);
//赋值
acdt.rollAngle = angle[0];
acdt.pitchAngle = angle[1];
acdt.yawAngle = angle[2];
//发送数据
xQueueSend(AHRSToFlightConQueue,&acdt,0);
xQueueSend(AHRSToINSQueue,&p_insBuffer,0);
vTaskDelayUntil(&lastTime,(portTickType)(5/portTICK_RATE_MS));
}
}
/*
* para1 gyro rate
* para2 null
* para3 dt
* */
void AHRS_GetA(float *A,void *para1,void *para2,void *para3)
{
float *w=(float *)para1;
float DT=*(float *)para3 * 0.5;
A[0]=1.0; A[1]=-w[0]*DT; A[2]=-w[1]*DT; A[3]=-w[2]*DT;
A[4]=w[0]*DT; A[5]=1.0; A[6]=w[2]*DT; A[7]=-w[1]*DT;
A[8]=w[1]*DT; A[9]=-w[2]*DT; A[10]=1.0; A[11]=w[0]*DT;
A[12]=w[2]*DT; A[13]=w[1]*DT; A[14]=-w[0]*DT; A[15]=1.0;
}
void AHRS_GetH(float *H,void *para1,void *para2)
{
float *q=(float *)para1;
#ifdef MEASURE_DIM6
float *m0_=(float *)para2;
#endif
// float g=-9.814;
// g=-1;
float q2[4];
q2[0]=2*q[0];
q2[1]=2*q[1];
q2[2]=2*q[2];
q2[3]=2*q[3];
H[0]=q2[2]; H[1]=-q2[3]; H[2]=q2[0]; H[3]=-q2[1];
H[4]=-q2[1]; H[5]=-q2[0]; H[6]=-q2[3]; H[7]=-q2[2];
H[8]=-q2[0]; H[9]=q2[1]; H[10]=q2[2]; H[11]=-q2[3];
#ifdef MEASURE_DIM6
H[12]=m0_[0]*q2[0]-m0_[2]*q2[2]; H[13]=m0_[0]*q2[1]+m0_[2]*q2[3]; H[14]=-m0_[0]*q2[2]-m0_[2]*q2[0]; H[15]=-m0_[0]*q2[3]+m0_[2]*q2[1];
H[16]=-m0_[0]*q2[3]+m0_[2]*q2[1]; H[17]=m0_[0]*q2[2]+m0_[2]*q2[0]; H[18]=m0_[0]*q2[1]+m0_[2]*q2[3]; H[19]=-m0_[0]*q2[0]+m0_[2]*q2[2];
H[20]=m0_[0]*q2[2]+m0_[2]*q2[0]; H[21]=m0_[0]*q2[3]-m0_[2]*q2[1]; H[22]=m0_[0]*q2[0]-m0_[2]*q2[2]; H[23]= m0_[0]*q2[1]+m0_[2]*q2[3];
#endif
}
/*
* para1 matrix A
* para2 NULL
* */
void AHRS_aFunc(float *q,void *para1,void *para2)
{
float *A=(float *)para1;
arm_matrix_instance_f32 newqMat,qMat,AMat;
newqMat.numRows=4;
newqMat.numCols=1;
newqMat.pData=pvPortMalloc(4*sizeof(float));
qMat.numRows=4;
qMat.numCols=1;
qMat.pData=q;
AMat.numRows=4;
AMat.numCols=4;
AMat.pData=A;
arm_mat_mult_f32(&AMat,&qMat,&newqMat);
memcpy(q,newqMat.pData,4*sizeof(float));
vPortFree(newqMat.pData);
}
void AHRS_hFunc(float *hx,void *para1,void *para2)
{
float *q = (float *)para1;
float *m0_ = (float *)para2;
float g[3]={0.0, 0.0, -1};
arm_matrix_instance_f32 CbnMat,CnbMat
,gMat,m0Mat,hx1Mat,hx2Mat;
CbnMat.numRows=3;
CbnMat.numCols=3;
CbnMat.pData=pvPortMalloc(9*sizeof(float));
CnbMat.numRows=3;
CnbMat.numCols=3;
CnbMat.pData=pvPortMalloc(9*sizeof(float));
Quat2dcm(CbnMat.pData,q);
arm_mat_trans_f32(&CbnMat,&CnbMat);
// hx[3]=CbnMat.pData[0];
// hx[4]=CbnMat.pData[1];
// hx[5]=CbnMat.pData[2];
vPortFree(CbnMat.pData);
hx1Mat.numRows=3;
hx1Mat.numCols=1;
hx1Mat.pData=pvPortMalloc(3*sizeof(float));
gMat.numRows=3;
gMat.numCols=1;
gMat.pData=g;
arm_mat_mult_f32(&CnbMat,&gMat,&hx1Mat);
hx2Mat.numRows=3;
hx2Mat.numCols=1;
hx2Mat.pData=pvPortMalloc(3*sizeof(float));
m0Mat.numRows=3;
m0Mat.numCols=1;
m0Mat.pData=m0_;
#ifdef MEASURE_DIM6
arm_mat_mult_f32(&CnbMat,&m0Mat,&hx2Mat);
#endif
vPortFree(CnbMat.pData);
hx[0]=hx1Mat.pData[0];
hx[1]=hx1Mat.pData[1];
hx[2]=hx1Mat.pData[2];
#ifdef MEASURE_DIM6
hx[3]=hx2Mat.pData[0];
hx[4]=hx2Mat.pData[1];
hx[5]=hx2Mat.pData[2];
#endif
vPortFree(hx1Mat.pData);
vPortFree(hx2Mat.pData);
}