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https://gitee.com/dlmu-cone/bf_original_balance_chassis
synced 2026-07-24 03:27:45 +08:00
重新组织了文件的防止
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@@ -57,7 +57,7 @@ attitude_t *INS_Init(void)
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IMU_QuaternionEKF_Init(10, 0.001, 10000000, 1, 0);
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// imu heat init
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PID_Init_config_s config = {.MaxOut = 2000,
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PID_Init_Config_s config = {.MaxOut = 2000,
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.IntegralLimit = 300,
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.DeadBand = 0,
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.Kp = 1000,
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@@ -68,7 +68,7 @@ attitude_t *INS_Init(void)
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// noise of accel is relatively big and of high freq,thus lpf is used
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INS.AccelLPF = 0.0085;
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return (attitude_t*)&INS.Roll;
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return (attitude_t*)&INS.Gyro; // @todo: 这里偷懒了,不要这样做! 修改INT_t结构体可能会导致异常,待修复.
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}
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/* 注意以1kHz的频率运行此任务 */
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@@ -96,8 +96,8 @@ void INS_Task(void)
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IMU_Param_Correction(&IMU_Param, INS.Gyro, INS.Accel);
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// 计算重力加速度矢量和b系的XY两轴的夹角,可用作功能扩展,本demo暂时没用
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INS.atanxz = -atan2f(INS.Accel[X], INS.Accel[Z]) * 180 / PI;
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INS.atanyz = atan2f(INS.Accel[Y], INS.Accel[Z]) * 180 / PI;
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// INS.atanxz = -atan2f(INS.Accel[X], INS.Accel[Z]) * 180 / PI;
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// INS.atanyz = atan2f(INS.Accel[Y], INS.Accel[Z]) * 180 / PI;
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// 核心函数,EKF更新四元数
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IMU_QuaternionEKF_Update(INS.Gyro[X], INS.Gyro[Y], INS.Gyro[Z], INS.Accel[X], INS.Accel[Y], INS.Accel[Z], dt);
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