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modules/imu/ins_task.h
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80
modules/imu/ins_task.h
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/**
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******************************************************************************
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* @file ins_task.h
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* @author Wang Hongxi
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* @version V2.0.0
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* @date 2022/2/23
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* @brief
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******************************************************************************
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* @attention
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*
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******************************************************************************
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*/
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#ifndef __INS_TASK_H
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#define __INS_TASK_H
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#include "stdint.h"
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#include "BMI088driver.h"
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#include "QuaternionEKF.h"
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#define X 0
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#define Y 1
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#define Z 2
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#define INS_TASK_PERIOD 1
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typedef struct
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{
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float q[4]; // 四元数估计值
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float Gyro[3]; // 角速度
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float Accel[3]; // 加速度
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float MotionAccel_b[3]; // 机体坐标加速度
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float MotionAccel_n[3]; // 绝对系加速度
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float AccelLPF; // 加速度低通滤波系数
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// 加速度在绝对系的向量表示
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float xn[3];
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float yn[3];
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float zn[3];
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float atanxz;
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float atanyz;
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// 位姿
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float Roll;
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float Pitch;
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float Yaw;
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float YawTotalAngle;
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} INS_t;
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/**
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* @brief 用于修正安装误差的参数,demo中可无视
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*
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*/
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typedef struct
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{
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uint8_t flag;
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float scale[3];
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float Yaw;
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float Pitch;
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float Roll;
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} IMU_Param_t;
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extern INS_t INS;
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void INS_Init(void);
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void INS_Task(void);
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void IMU_Temperature_Ctrl(void);
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void QuaternionUpdate(float *q, float gx, float gy, float gz, float dt);
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void QuaternionToEularAngle(float *q, float *Yaw, float *Pitch, float *Roll);
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void EularAngleToQuaternion(float Yaw, float Pitch, float Roll, float *q);
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void BodyFrameToEarthFrame(const float *vecBF, float *vecEF, float *q);
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void EarthFrameToBodyFrame(const float *vecEF, float *vecBF, float *q);
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#endif
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