mirror of
https://gitee.com/dlmu-cone/half-steering-basic-framework
synced 2026-10-24 01:52:20 +08:00
@@ -12,7 +12,7 @@ set(CMAKE_OBJCOPY arm-none-eabi-objcopy)
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set(CMAKE_OBJDUMP arm-none-eabi-objdump)
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set(CMAKE_OBJDUMP arm-none-eabi-objdump)
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set(SIZE arm-none-eabi-size)
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set(SIZE arm-none-eabi-size)
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set(CMAKE_AR arm-none-eabi-ar)
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set(CMAKE_AR arm-none-eabi-ar)
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set(CMAKE_C_STANDARD 11)
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set(CMAKE_C_STANDARD 23)
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set(CMAKE_EXPORT_COMPILE_COMMANDS ON)
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set(CMAKE_EXPORT_COMPILE_COMMANDS ON)
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# 指定工程名称和语言类型
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# 指定工程名称和语言类型
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@@ -1,4 +1,4 @@
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# YueLu2022/2023 EC basic_framework-dev
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# basic_framework-dev
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湖南大学RoboMaster跃鹿战队2022-2023电控通用嵌入式框架。
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湖南大学RoboMaster跃鹿战队2022-2023电控通用嵌入式框架。
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@@ -56,15 +56,15 @@ static referee_info_t* referee_data; // 用于获取裁判系统的数据
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static Referee_Interactive_info_t ui_data; // UI数据,将底盘中的数据传入此结构体的对应变量中,UI会自动检测是否变化,对应显示UI
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static Referee_Interactive_info_t ui_data; // UI数据,将底盘中的数据传入此结构体的对应变量中,UI会自动检测是否变化,对应显示UI
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static SuperCapInstance *cap; // 超级电容
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static SuperCapInstance *cap; // 超级电容
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static LKMotorInstance *motor_lf,*motor_rb; // 轮电机9015
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static LKMotorInstance *motor_lb,*motor_rf; // 轮电机9015
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static DJIMotorInstance *motor_steering_lf,*motor_steering_rb; // 舵电机6020
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static DJIMotorInstance *motor_steering_lb,*motor_steering_rf; // 舵电机6020
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/* 用于自旋变速策略的时间变量 */
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/* 用于自旋变速策略的时间变量 */
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// static float t;
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// static float t;
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/* 私有函数计算的中介变量,设为静态避免参数传递的开销 */
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/* 私有函数计算的中介变量,设为静态避免参数传递的开销 */
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static float chassis_vx, chassis_vy; // 将云台系的速度投影到底盘
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static float chassis_vx, chassis_vy; // 将云台系的速度投影到底盘
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static float vt_lf, vt_rb; // 底盘速度解算后的临时输出,待进行限幅
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static float vt_lb, vt_rf; // 底盘速度解算后的临时输出,待进行限幅
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static float at_lf, at_rb; // 底盘的角度解算后的临时输出,待进行限幅
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static float at_lb, at_rf; // 底盘的角度解算后的临时输出,待进行限幅
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static PIDInstance chassis_follow_pid; // 底盘跟随云台的PID
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static PIDInstance chassis_follow_pid; // 底盘跟随云台的PID
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void ChassisInit()
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void ChassisInit()
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@@ -102,11 +102,11 @@ void ChassisInit()
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chassis_motor_config.can_init_config.tx_id = 1;
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chassis_motor_config.can_init_config.tx_id = 1;
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// chassis_motor_config.controller_setting_init_config.motor_reverse_flag = MOTOR_DIRECTION_REVERSE;
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// chassis_motor_config.controller_setting_init_config.motor_reverse_flag = MOTOR_DIRECTION_REVERSE;
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motor_rb = LKMotorInit(&chassis_motor_config);
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motor_rf = LKMotorInit(&chassis_motor_config);
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chassis_motor_config.can_init_config.tx_id = 2;
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chassis_motor_config.can_init_config.tx_id = 2;
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// chassis_motor_config.controller_setting_init_config.motor_reverse_flag = MOTOR_DIRECTION_REVERSE;
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// chassis_motor_config.controller_setting_init_config.motor_reverse_flag = MOTOR_DIRECTION_REVERSE;
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motor_lf = LKMotorInit(&chassis_motor_config);
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motor_lb = LKMotorInit(&chassis_motor_config);
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// 舵电机6020初始化
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// 舵电机6020初始化
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Motor_Init_Config_s chassis_motor_steering_config = {
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Motor_Init_Config_s chassis_motor_steering_config = {
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@@ -145,16 +145,16 @@ void ChassisInit()
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};
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};
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chassis_motor_steering_config.can_init_config.tx_id = 1;
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chassis_motor_steering_config.can_init_config.tx_id = 1;
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motor_steering_rb = DJIMotorInit(&chassis_motor_steering_config);
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motor_steering_rf = DJIMotorInit(&chassis_motor_steering_config);
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chassis_motor_steering_config.can_init_config.tx_id = 2;
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chassis_motor_steering_config.can_init_config.tx_id = 2;
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motor_steering_lf = DJIMotorInit(&chassis_motor_steering_config);
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motor_steering_lb = DJIMotorInit(&chassis_motor_steering_config);
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PID_Init_Config_s chassis_follow_pid_conf = {
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PID_Init_Config_s chassis_follow_pid_conf = {
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.Kp = 20, // 6
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.Kp = 1.05, // 6
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.Ki = 0,
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.Ki = 0,
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.Kd = 3, // 0.5
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.Kd = 0.1, // 0.495
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.DeadBand = 0.5f,
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.DeadBand = 0.5f,// 启用死区,值为0.5度
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//.CoefA = 0.2,
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//.CoefA = 0.2,
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//.CoefB = 0.3,
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//.CoefB = 0.3,
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//.Improve = PID_Trapezoid_Intergral | PID_DerivativeFilter | PID_DerivativeFilter | PID_Derivative_On_Measurement | PID_Integral_Limit | PID_Derivative_On_Measurement,
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//.Improve = PID_Trapezoid_Intergral | PID_DerivativeFilter | PID_DerivativeFilter | PID_Derivative_On_Measurement | PID_Integral_Limit | PID_Derivative_On_Measurement,
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@@ -232,7 +232,7 @@ static void MinmizeRotation(float *angle, const float *last_angle, float *speed)
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while (norm_rotation < -180.0f) {
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while (norm_rotation < -180.0f) {
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norm_rotation += 360.0f;
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norm_rotation += 360.0f;
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}
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}
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float threshold = 90.0f;
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float threshold = 110.0f;
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float target_single=fmodf(target_angle,360.0f);
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float target_single=fmodf(target_angle,360.0f);
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if(target_single<0.0f) target_single+=360.0f;
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if(target_single<0.0f) target_single+=360.0f;
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@@ -240,16 +240,16 @@ static void MinmizeRotation(float *angle, const float *last_angle, float *speed)
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if(current_single<0.0f) current_single+=360.0f;
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if(current_single<0.0f) current_single+=360.0f;
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if (fabsf(norm_rotation) > threshold) {
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if (norm_rotation > threshold) {
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int32_t round_diff = (int32_t)(target_angle / 360.0f) - (int32_t)(actual_angle / 360.0f);
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int32_t round_diff = (int32_t)((target_angle-actual_angle) / 360.0f);
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*angle = actual_angle + norm_rotation-180.0f+round_diff*360.0f;
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*angle = actual_angle + norm_rotation-180.0f+round_diff*360.0f;
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*speed = -(*speed);
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*speed = -(*speed);
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}else if(norm_rotation<-threshold){
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}else if(norm_rotation<-threshold){
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int32_t round_diff = (int32_t)(target_angle / 360.0f) - (int32_t)(actual_angle / 360.0f);
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int32_t round_diff = (int32_t)((target_angle-actual_angle) / 360.0f);
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*angle = actual_angle + norm_rotation+180.0f+round_diff*360.0f;
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*angle = actual_angle + norm_rotation+180.0f+round_diff*360.0f;
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*speed = -(*speed);
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*speed = -(*speed);
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}
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}
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ANGLE_LIMIT_360_TO_180_ABS(*angle);
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// ANGLE_LIMIT_360_TO_180_ABS(*angle);
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// float rotation = *angle - *last_angle;
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// float rotation = *angle - *last_angle;
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// ANGLE_LIMIT_360_TO_180_ABS(rotation);
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// ANGLE_LIMIT_360_TO_180_ABS(rotation);
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// if (rotation > 90) {
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// if (rotation > 90) {
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@@ -268,44 +268,57 @@ static void MinmizeRotation(float *angle, const float *last_angle, float *speed)
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*/
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*/
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static void SteeringWheelCalculate()
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static void SteeringWheelCalculate()
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{
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{
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float offset_lf, offset_rb; // 用于计算舵轮的角度
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float offset_rf, offset_lb; // 用于计算舵轮的角度
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float at_lf_last, at_rb_last; // 上次的角度
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float at_rf_last, at_lb_last; // 上次的角度
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at_lf_last = motor_steering_lf->measure.total_angle;
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at_lb_last = motor_steering_lb->measure.total_angle;
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at_rb_last = motor_steering_rb->measure.total_angle;
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// at_lf_last = motor_steering_lf->measure.total_angle;
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at_rf_last = motor_steering_rf->measure.total_angle;
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// at_rb_last = motor_steering_rb->measure.total_angle;
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if (chassis_vx == 0 && chassis_vy == 0 && chassis_cmd_recv.wz == 0) {
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if (chassis_vx == 0 && chassis_vy == 0 && chassis_cmd_recv.wz == 0) {
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// at_lf = at_lf_last;
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// at_lf = at_lf_last;
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// at_rf = at_rf_last;
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// at_rf = at_rf_last;
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// at_lb = at_lb_last;
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// at_lb = at_lb_last;
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// at_rb = at_rb_last;
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// at_rb = at_rb_last;
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vt_lf = 0, vt_rb = 0;
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vt_lb = 0, vt_rf = 0;
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} else {
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} else {
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// 生成预计算变量,减少计算量,空间换时间
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// 生成预计算变量,减少计算量,空间换时间
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float w = chassis_cmd_recv.wz * CHASSIS_WHEEL_OFFSET * SQRT2;
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float w = chassis_cmd_recv.wz * CHASSIS_WHEEL_OFFSET * SQRT2;
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float temp_x = chassis_vx - w, temp_y = chassis_vy - w;
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float temp_x = chassis_vx - w, temp_y = chassis_vy - w;
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arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_lf); // lf:y- , x-
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// arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_lf); // lf:y- , x-
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temp_y = chassis_vy + w; // 重复利用变量,temp_x = chassis_vy - w;与上次相同因此注释
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// temp_y = chassis_vy + w; // 重复利用变量,temp_x = chassis_vy - w;与上次相同因此注释
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// arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_lb); // lb: y+ , x-
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arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_lb); // lb: y+ , x-
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// temp_x = chassis_vx + w; // temp_y = chassis_vx + w;与上次相同因此注释
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temp_x = chassis_vx + w;
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arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_rb); // rb: y+ , x+
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temp_y = chassis_vy + w;//与上次相同因此注释
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temp_y = chassis_vy - w; // temp_x = chassis_vy + w;与上次相同因此注释
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// arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_rb); // rb: y+ , x+
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// arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_rf); // rf: y- , x+
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// temp_y = chassis_vy - w; // temp_x = chassis_vy + w;与上次相同因此注释
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arm_sqrt_f32(temp_x * temp_x + temp_y * temp_y, &vt_rf); // rf: y- , x+
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// 计算角度偏移
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// 计算角度偏移
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offset_lf = atan2f(chassis_vx - w, chassis_vy - w) * RAD_2_DEGREE; // lf: y- , x-
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// offset_lf = atan2f(chassis_vy - w, chassis_vx - w) * RAD_2_DEGREE; // lf: y- , x-
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offset_rb = atan2f(chassis_vx + w, chassis_vy + w) * RAD_2_DEGREE; // rb: y+ , x+
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offset_rf = atan2f(chassis_vy - w, chassis_vx - w) * RAD_2_DEGREE; // rf: y- , x+
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offset_lb = atan2f(chassis_vy + w, chassis_vx + w) * RAD_2_DEGREE; // lb: y+ , x-注意
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// offset_rb = atan2f(chassis_vy + w, chassis_vx + w) * RAD_2_DEGREE; // rb: y+ , x+
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at_lf = STEERING_CHASSIS_ALIGN_ANGLE_LF + offset_lf; // 此处似乎不需要加上真实角度,因为我们需要的是绝对角度而不是相对角度
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// at_lf = STEERING_CHASSIS_ALIGN_ANGLE_LF + offset_lf; // 此处似乎不需要加上真实角度,因为我们需要的是绝对角度而不是相对角度
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at_rb = STEERING_CHASSIS_ALIGN_ANGLE_RB + offset_rb;
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at_rf = STEERING_CHASSIS_ALIGN_ANGLE_RF + offset_rf;
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at_lb = STEERING_CHASSIS_ALIGN_ANGLE_LB + offset_lb;
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// at_rb = STEERING_CHASSIS_ALIGN_ANGLE_RB + offset_rb;
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ANGLE_LIMIT_360_TO_180_ABS(at_lf);
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// ANGLE_LIMIT_360_TO_180_ABS(at_lf);
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ANGLE_LIMIT_360_TO_180_ABS(at_rb);
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ANGLE_LIMIT_360_TO_180_ABS(at_rf);
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ANGLE_LIMIT_360_TO_180_ABS(at_lb);
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// ANGLE_LIMIT_360_TO_180_ABS(at_rb);
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MinmizeRotation(&at_lf, &at_lf_last, &vt_lf);
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// MinmizeRotation(&at_lf, &at_lf_last, &vt_lf);
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MinmizeRotation(&at_rb, &at_rb_last, &vt_rb);
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MinmizeRotation(&at_rf, &at_rf_last, &vt_rf);
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MinmizeRotation(&at_lb, &at_lb_last, &vt_lb);
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// MinmizeRotation(&at_rb, &at_rb_last, &vt_rb);
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}
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}
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DJIMotorSetRef(motor_steering_lf, at_lf);
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// DJIMotorSetRef(motor_steering_lf, at_lf);
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DJIMotorSetRef(motor_steering_rb, at_rb);
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DJIMotorSetRef(motor_steering_rf, at_rf);
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DJIMotorSetRef(motor_steering_lb, at_lb);
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// DJIMotorSetRef(motor_steering_rb, at_rb);
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}
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}
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/**
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/**
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@@ -335,8 +348,8 @@ static void LimitChassisOutput()
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// LKMotorSetRef( motor_lf , vt_lf );
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// LKMotorSetRef( motor_lf , vt_lf );
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// LKMotorSetRef( motor_rb , vt_rb );
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// LKMotorSetRef( motor_rb , vt_rb );
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LKMotorSetRef( motor_lf , vt_lf );
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LKMotorSetRef( motor_rf , vt_rf );
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LKMotorSetRef( motor_rb , vt_rb );
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LKMotorSetRef( motor_lb , vt_lb );
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}
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}
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/**
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/**
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@@ -365,18 +378,18 @@ void ChassisTask()
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if (chassis_cmd_recv.chassis_mode == CHASSIS_ZERO_FORCE)
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if (chassis_cmd_recv.chassis_mode == CHASSIS_ZERO_FORCE)
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{ // 如果出现重要模块离线或遥控器设置为急停,让电机停止
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{ // 如果出现重要模块离线或遥控器设置为急停,让电机停止
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LKMotorStop(motor_lf);
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LKMotorStop(motor_rf);
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LKMotorStop(motor_rb);
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LKMotorStop(motor_lb);
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DJIMotorStop(motor_steering_lf);
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DJIMotorStop(motor_steering_rf);
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DJIMotorStop(motor_steering_rb);
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DJIMotorStop(motor_steering_lb);
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}
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}
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else
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else
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{
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{
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// 正常工作
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// 正常工作
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LKMotorEnable(motor_lf);
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LKMotorEnable(motor_rf);
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LKMotorEnable(motor_rb);
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LKMotorEnable(motor_lb);
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DJIMotorEnable(motor_steering_lf);
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DJIMotorEnable(motor_steering_rf);
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DJIMotorEnable(motor_steering_rb);
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DJIMotorEnable(motor_steering_lb);
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}
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}
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// 根据控制模式设定旋转速度
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// 根据控制模式设定旋转速度
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@@ -386,8 +399,8 @@ void ChassisTask()
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chassis_cmd_recv.wz = 0;
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chassis_cmd_recv.wz = 0;
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break;
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break;
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case CHASSIS_FOLLOW_GIMBAL_YAW: // 跟随云台,不单独设置pid,以误差角度平方为速度输出
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case CHASSIS_FOLLOW_GIMBAL_YAW: // 跟随云台,不单独设置pid,以误差角度平方为速度输出
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// float single_round_offset = chassis_cmd_recv.offset_angle;
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float single_round_offset = chassis_cmd_recv.offset_angle;
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float single_round_offset = chassis_cmd_recv.offset_angle;
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// float single_round_offset = fmodf(chassis_cmd_recv.offset_angle, 360.0f);
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if(single_round_offset > 180.0f)
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if(single_round_offset > 180.0f)
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{
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{
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single_round_offset -= 360.0f;
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single_round_offset -= 360.0f;
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@@ -395,7 +408,6 @@ void ChassisTask()
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else if(single_round_offset < -180.0f)
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else if(single_round_offset < -180.0f)
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{
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{
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single_round_offset += 360.0f;
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single_round_offset += 360.0f;
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}
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}
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chassis_cmd_recv.wz = PIDCalculate(&chassis_follow_pid, single_round_offset, 0)/100;
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chassis_cmd_recv.wz = PIDCalculate(&chassis_follow_pid, single_round_offset, 0)/100;
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||||||
// chassis_cmd_recv.wz = PIDCalculate(&chassis_follow_pid, chassis_cmd_recv.offset_angle, 0)/100;
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// chassis_cmd_recv.wz = PIDCalculate(&chassis_follow_pid, chassis_cmd_recv.offset_angle, 0)/100;
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@@ -413,7 +425,7 @@ void ChassisTask()
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|||||||
cos_theta = arm_cos_f32(chassis_cmd_recv.offset_angle * DEGREE_2_RAD);
|
cos_theta = arm_cos_f32(chassis_cmd_recv.offset_angle * DEGREE_2_RAD);
|
||||||
sin_theta = arm_sin_f32(chassis_cmd_recv.offset_angle * DEGREE_2_RAD);
|
sin_theta = arm_sin_f32(chassis_cmd_recv.offset_angle * DEGREE_2_RAD);
|
||||||
chassis_vx = chassis_cmd_recv.vx * cos_theta - chassis_cmd_recv.vy * sin_theta;
|
chassis_vx = chassis_cmd_recv.vx * cos_theta - chassis_cmd_recv.vy * sin_theta;
|
||||||
chassis_vy = chassis_cmd_recv.vx * sin_theta + chassis_cmd_recv.vy * cos_theta;
|
chassis_vy = -chassis_cmd_recv.vx * sin_theta - chassis_cmd_recv.vy * cos_theta;
|
||||||
|
|
||||||
// 根据控制模式进行正运动学解算,计算底盘输出
|
// 根据控制模式进行正运动学解算,计算底盘输出
|
||||||
SteeringWheelCalculate();
|
SteeringWheelCalculate();
|
||||||
|
|||||||
@@ -15,7 +15,7 @@
|
|||||||
// 私有宏,自动将编码器转换成角度值
|
// 私有宏,自动将编码器转换成角度值
|
||||||
#define YAW_ALIGN_ANGLE (YAW_CHASSIS_ALIGN_ECD * ECD_ANGLE_COEF_DJI) // 对齐时的角度,0-360
|
#define YAW_ALIGN_ANGLE (YAW_CHASSIS_ALIGN_ECD * ECD_ANGLE_COEF_DJI) // 对齐时的角度,0-360
|
||||||
#define PTICH_HORIZON_ANGLE (PITCH_HORIZON_ECD * ECD_ANGLE_COEF_DJI) // pitch水平时电机的角度,0-360
|
#define PTICH_HORIZON_ANGLE (PITCH_HORIZON_ECD * ECD_ANGLE_COEF_DJI) // pitch水平时电机的角度,0-360
|
||||||
|
uint16_t around=0;
|
||||||
/* cmd应用包含的模块实例指针和交互信息存储*/
|
/* cmd应用包含的模块实例指针和交互信息存储*/
|
||||||
#ifdef GIMBAL_BOARD // 对双板的兼容,条件编译
|
#ifdef GIMBAL_BOARD // 对双板的兼容,条件编译
|
||||||
#include "can_comm.h"
|
#include "can_comm.h"
|
||||||
@@ -30,8 +30,8 @@ static Chassis_Ctrl_Cmd_s chassis_cmd_send; // 发送给底盘应用的信
|
|||||||
static Chassis_Upload_Data_s chassis_fetch_data; // 从底盘应用接收的反馈信息信息,底盘功率枪口热量与底盘运动状态等
|
static Chassis_Upload_Data_s chassis_fetch_data; // 从底盘应用接收的反馈信息信息,底盘功率枪口热量与底盘运动状态等
|
||||||
|
|
||||||
static RC_ctrl_t *rc_data; // 遥控器数据,初始化时返回
|
static RC_ctrl_t *rc_data; // 遥控器数据,初始化时返回
|
||||||
static Vision_Recv_s *vision_recv_data; // 视觉接收数据指针,初始化时返回
|
// static Vision_Recv_s *vision_recv_data; // 视觉接收数据指针,初始化时返回
|
||||||
static Vision_Send_s vision_send_data; // 视觉发送数据
|
// static Vision_Send_s vision_send_data; // 视觉发送数据
|
||||||
|
|
||||||
static Publisher_t *gimbal_cmd_pub; // 云台控制消息发布者
|
static Publisher_t *gimbal_cmd_pub; // 云台控制消息发布者
|
||||||
static Subscriber_t *gimbal_feed_sub; // 云台反馈信息订阅者
|
static Subscriber_t *gimbal_feed_sub; // 云台反馈信息订阅者
|
||||||
@@ -48,7 +48,7 @@ static Robot_Status_e robot_state; // 机器人整体工作状态
|
|||||||
void RobotCMDInit()
|
void RobotCMDInit()
|
||||||
{
|
{
|
||||||
rc_data = RemoteControlInit(&huart3); // 修改为对应串口,注意如果是自研板dbus协议串口需选用添加了反相器的那个
|
rc_data = RemoteControlInit(&huart3); // 修改为对应串口,注意如果是自研板dbus协议串口需选用添加了反相器的那个
|
||||||
vision_recv_data = VisionInit(&huart1); // 视觉通信串口
|
// vision_recv_data = VisionInit(&huart1); // 视觉通信串口
|
||||||
|
|
||||||
gimbal_cmd_pub = PubRegister("gimbal_cmd", sizeof(Gimbal_Ctrl_Cmd_s));
|
gimbal_cmd_pub = PubRegister("gimbal_cmd", sizeof(Gimbal_Ctrl_Cmd_s));
|
||||||
gimbal_feed_sub = SubRegister("gimbal_feed", sizeof(Gimbal_Upload_Data_s));
|
gimbal_feed_sub = SubRegister("gimbal_feed", sizeof(Gimbal_Upload_Data_s));
|
||||||
@@ -80,13 +80,26 @@ void RobotCMDInit()
|
|||||||
* @brief 根据gimbal app传回的当前电机角度计算和零位的误差
|
* @brief 根据gimbal app传回的当前电机角度计算和零位的误差
|
||||||
* 单圈绝对角度的范围是0~360,说明文档中有图示
|
* 单圈绝对角度的范围是0~360,说明文档中有图示
|
||||||
*
|
*
|
||||||
*/
|
*///static float base_total_angle = 0.0f; // 用于计算偏移的基准角度
|
||||||
static void CalcOffsetAngle()
|
static void CalcOffsetAngle()
|
||||||
{
|
{
|
||||||
static float last_offset_angle = 0;
|
static float last_offset_angle = 0;
|
||||||
const float smooth_factor = 0.3f; // 平滑因子,0~1之间,值越大平滑效果越明显
|
const float smooth_factor = 0.3f; // 平滑因子,0~1之间,值越大平滑效果越明显
|
||||||
|
|
||||||
|
const float deadband = 3.0f; // 死区值
|
||||||
|
// 新增:跟踪模式变化,用于重置基准角度
|
||||||
|
// static chassis_mode_e last_chassis_mode = CHASSIS_NO_FOLLOW;//
|
||||||
|
//
|
||||||
|
//
|
||||||
|
// // 当从旋转模式切换到跟随模式时,重置基准角度
|
||||||
|
// if (last_chassis_mode == CHASSIS_ROTATE && chassis_cmd_send.chassis_mode == CHASSIS_FOLLOW_GIMBAL_YAW)
|
||||||
|
// {
|
||||||
|
// base_total_angle = gimbal_fetch_data.yaw_motor_total_angle;
|
||||||
|
// last_offset_angle = 0.0f; // 同时重置历史偏移值
|
||||||
|
// }
|
||||||
|
|
||||||
float new_offset = gimbal_fetch_data.yaw_motor_total_angle - YAW_ALIGN_ANGLE;
|
float new_offset = gimbal_fetch_data.yaw_motor_total_angle - YAW_ALIGN_ANGLE;
|
||||||
#if YAW_CHASSIS_REVERSE
|
#if YAW_ECD_GREATER_THAN_4096
|
||||||
new_offset = -new_offset;
|
new_offset = -new_offset;
|
||||||
#endif
|
#endif
|
||||||
float angle_diff = new_offset - last_offset_angle;
|
float angle_diff = new_offset - last_offset_angle;
|
||||||
@@ -94,8 +107,25 @@ static void CalcOffsetAngle()
|
|||||||
new_offset -= 360.0f;
|
new_offset -= 360.0f;
|
||||||
else if (angle_diff < -180.0f)
|
else if (angle_diff < -180.0f)
|
||||||
new_offset += 360.0f;
|
new_offset += 360.0f;
|
||||||
|
/////
|
||||||
|
// 应用死区
|
||||||
|
if (fabs(new_offset) < deadband) {
|
||||||
|
new_offset = 0.0f;
|
||||||
|
} else if (new_offset > 0) {
|
||||||
|
new_offset -= deadband;
|
||||||
|
} else {
|
||||||
|
new_offset += deadband;
|
||||||
|
}//////
|
||||||
chassis_cmd_send.offset_angle = last_offset_angle *(1.0f - smooth_factor) + new_offset * smooth_factor;
|
chassis_cmd_send.offset_angle = last_offset_angle *(1.0f - smooth_factor) + new_offset * smooth_factor;
|
||||||
last_offset_angle = chassis_cmd_send.offset_angle;
|
last_offset_angle = chassis_cmd_send.offset_angle;
|
||||||
|
// // 更新模式状态
|
||||||
|
// last_chassis_mode = chassis_cmd_send.chassis_mode;
|
||||||
|
// // 当处于旋转模式时,更新基准角度以防止累积过大误差
|
||||||
|
// if (chassis_cmd_send.chassis_mode == CHASSIS_ROTATE)
|
||||||
|
// {
|
||||||
|
// base_total_angle = gimbal_fetch_data.yaw_motor_total_angle;
|
||||||
|
// }
|
||||||
|
|
||||||
// static float angle;
|
// static float angle;
|
||||||
// static float last_diff = 0.0f; // 用于在±180°附近保持上次符号,避免来回跳变
|
// static float last_diff = 0.0f; // 用于在±180°附近保持上次符号,避免来回跳变
|
||||||
// /* 使用 yaw 电机的单圈角度与 `YAW_ALIGN_ANGLE` 对齐(保持原实现的参考系)
|
// /* 使用 yaw 电机的单圈角度与 `YAW_ALIGN_ANGLE` 对齐(保持原实现的参考系)
|
||||||
@@ -151,11 +181,15 @@ static void RemoteControlSet()
|
|||||||
// 控制底盘和云台运行模式,云台待添加,云台是否始终使用IMU数据?
|
// 控制底盘和云台运行模式,云台待添加,云台是否始终使用IMU数据?
|
||||||
if (switch_is_up(rc_data[TEMP].rc.switch_right)) // 右侧开关状态[下],底盘跟随云台
|
if (switch_is_up(rc_data[TEMP].rc.switch_right)) // 右侧开关状态[下],底盘跟随云台
|
||||||
{
|
{
|
||||||
|
// around = 0;
|
||||||
chassis_cmd_send.chassis_mode = CHASSIS_ROTATE;
|
chassis_cmd_send.chassis_mode = CHASSIS_ROTATE;
|
||||||
gimbal_cmd_send.gimbal_mode = GIMBAL_GYRO_MODE;
|
gimbal_cmd_send.gimbal_mode = GIMBAL_GYRO_MODE;
|
||||||
|
around= chassis_cmd_send.offset_angle/360;
|
||||||
}
|
}
|
||||||
else if (switch_is_mid(rc_data[TEMP].rc.switch_right)) // 右侧开关状态[中],底盘和云台分离,底盘保持不转动
|
else if (switch_is_mid(rc_data[TEMP].rc.switch_right)) // 右侧开关状态[中],底盘和云台分离,底盘保持不转动
|
||||||
{
|
{
|
||||||
|
//gimbal_fetch_data.yaw_motor_total_angle = gimbal_fetch_data.yaw_motor_total_angle-around*360;
|
||||||
|
chassis_cmd_send.offset_angle = chassis_cmd_send.offset_angle - 360*around;
|
||||||
chassis_cmd_send.chassis_mode = CHASSIS_FOLLOW_GIMBAL_YAW;
|
chassis_cmd_send.chassis_mode = CHASSIS_FOLLOW_GIMBAL_YAW;
|
||||||
gimbal_cmd_send.gimbal_mode = GIMBAL_GYRO_MODE;
|
gimbal_cmd_send.gimbal_mode = GIMBAL_GYRO_MODE;
|
||||||
}
|
}
|
||||||
@@ -167,7 +201,7 @@ static void RemoteControlSet()
|
|||||||
// ...
|
// ...
|
||||||
}
|
}
|
||||||
// 左侧开关状态为[下],或视觉未识别到目标,纯遥控器拨杆控制
|
// 左侧开关状态为[下],或视觉未识别到目标,纯遥控器拨杆控制
|
||||||
if (switch_is_down(rc_data[TEMP].rc.switch_left) || vision_recv_data->target_state == NO_TARGET)
|
if (switch_is_down(rc_data[TEMP].rc.switch_left) )
|
||||||
{ // 按照摇杆的输出大小进行角度增量,增益系数需调整
|
{ // 按照摇杆的输出大小进行角度增量,增益系数需调整
|
||||||
gimbal_cmd_send.yaw += 0.005f * (float)rc_data[TEMP].rc.rocker_l_;
|
gimbal_cmd_send.yaw += 0.005f * (float)rc_data[TEMP].rc.rocker_l_;
|
||||||
gimbal_cmd_send.pitch += 0.001f * (float)rc_data[TEMP].rc.rocker_l1;
|
gimbal_cmd_send.pitch += 0.001f * (float)rc_data[TEMP].rc.rocker_l1;
|
||||||
@@ -175,8 +209,8 @@ static void RemoteControlSet()
|
|||||||
// 云台软件限位
|
// 云台软件限位
|
||||||
|
|
||||||
// 底盘参数,目前没有加入小陀螺(调试似乎暂时没有必要),系数需要调整
|
// 底盘参数,目前没有加入小陀螺(调试似乎暂时没有必要),系数需要调整
|
||||||
chassis_cmd_send.vy = -0.15f * (float)rc_data[TEMP].rc.rocker_r_; // _水平方向
|
chassis_cmd_send.vx = 0.15f * (float)rc_data[TEMP].rc.rocker_r_; // _水平方向
|
||||||
chassis_cmd_send.vx = 0.15f * (float)rc_data[TEMP].rc.rocker_r1; // 1数值方向
|
chassis_cmd_send.vy = 0.15f * (float)rc_data[TEMP].rc.rocker_r1; // 1数值方向
|
||||||
|
|
||||||
// // 发射参数
|
// // 发射参数
|
||||||
// if (switch_is_up(rc_data[TEMP].rc.switch_right)) // 右侧开关状态[上],弹舱打开
|
// if (switch_is_up(rc_data[TEMP].rc.switch_right)) // 右侧开关状态[上],弹舱打开
|
||||||
@@ -347,5 +381,5 @@ void RobotCMDTask()
|
|||||||
#endif // GIMBAL_BOARD
|
#endif // GIMBAL_BOARD
|
||||||
PubPushMessage(shoot_cmd_pub, (void *)&shoot_cmd_send);
|
PubPushMessage(shoot_cmd_pub, (void *)&shoot_cmd_send);
|
||||||
PubPushMessage(gimbal_cmd_pub, (void *)&gimbal_cmd_send);
|
PubPushMessage(gimbal_cmd_pub, (void *)&gimbal_cmd_send);
|
||||||
VisionSend(&vision_send_data);
|
// VisionSend(&vision_send_data);
|
||||||
}
|
}
|
||||||
|
|||||||
@@ -26,8 +26,10 @@ void GimbalInit()
|
|||||||
},
|
},
|
||||||
.controller_param_init_config = {
|
.controller_param_init_config = {
|
||||||
.angle_PID = {
|
.angle_PID = {
|
||||||
|
//.Kp = 0.685, // 8
|
||||||
.Kp = 0.685, // 8
|
.Kp = 0.685, // 8
|
||||||
.Ki = 0.315,
|
//.Ki = 0.315,
|
||||||
|
.Ki = 0.25,
|
||||||
.Kd = 0.022,
|
.Kd = 0.022,
|
||||||
//.DeadBand = 0.1,
|
//.DeadBand = 0.1,
|
||||||
.Improve = PID_Trapezoid_Intergral | PID_Integral_Limit | PID_Derivative_On_Measurement | PID_DerivativeFilter | PID_ChangingIntegrationRate,
|
.Improve = PID_Trapezoid_Intergral | PID_Integral_Limit | PID_Derivative_On_Measurement | PID_DerivativeFilter | PID_ChangingIntegrationRate,
|
||||||
@@ -39,6 +41,7 @@ void GimbalInit()
|
|||||||
},
|
},
|
||||||
.speed_PID = {
|
.speed_PID = {
|
||||||
.Kp = 8000, // 50
|
.Kp = 8000, // 50
|
||||||
|
//.Kp = 5000, // 50
|
||||||
.Ki = 5000, // 200
|
.Ki = 5000, // 200
|
||||||
.Kd = 0,
|
.Kd = 0,
|
||||||
.CoefB = 1,
|
.CoefB = 1,
|
||||||
@@ -56,7 +59,7 @@ void GimbalInit()
|
|||||||
.speed_feedback_source = OTHER_FEED,
|
.speed_feedback_source = OTHER_FEED,
|
||||||
.outer_loop_type = ANGLE_LOOP,
|
.outer_loop_type = ANGLE_LOOP,
|
||||||
.close_loop_type = ANGLE_LOOP | SPEED_LOOP,
|
.close_loop_type = ANGLE_LOOP | SPEED_LOOP,
|
||||||
.motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
|
.motor_reverse_flag = MOTOR_DIRECTION_REVERSE,
|
||||||
},
|
},
|
||||||
.motor_type = GM6020};
|
.motor_type = GM6020};
|
||||||
// PITCH
|
// PITCH
|
||||||
@@ -93,7 +96,7 @@ void GimbalInit()
|
|||||||
.close_loop_type = SPEED_LOOP | ANGLE_LOOP,
|
.close_loop_type = SPEED_LOOP | ANGLE_LOOP,
|
||||||
.motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
|
.motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
|
||||||
},
|
},
|
||||||
.motor_type = GM6020,
|
.motor_type = M3508,
|
||||||
};
|
};
|
||||||
// 电机对total_angle闭环,上电时为零,会保持静止,收到遥控器数据再动
|
// 电机对total_angle闭环,上电时为零,会保持静止,收到遥控器数据再动
|
||||||
yaw_motor = DJIMotorInit(&yaw_config);
|
yaw_motor = DJIMotorInit(&yaw_config);
|
||||||
@@ -151,8 +154,9 @@ void GimbalTask()
|
|||||||
|
|
||||||
// 设置反馈数据,主要是imu和yaw的ecd
|
// 设置反馈数据,主要是imu和yaw的ecd
|
||||||
gimbal_feedback_data.gimbal_imu_data = *gimba_IMU_data;
|
gimbal_feedback_data.gimbal_imu_data = *gimba_IMU_data;
|
||||||
// gimbal_feedback_data.yaw_motor_single_round_angle = yaw_motor->measure.angle_single_round;
|
gimbal_feedback_data.yaw_motor_single_round_angle = yaw_motor->measure.angle_single_round;
|
||||||
gimbal_feedback_data.yaw_motor_single_round_angle = yaw_motor->measure.total_angle;
|
gimbal_feedback_data.yaw_motor_total_angle = yaw_motor->measure.total_angle;
|
||||||
|
// gimbal_feedback_data.yaw_motor_total_angle = gimba_IMU_data->YawTotalAngle;
|
||||||
// 推送消息
|
// 推送消息
|
||||||
PubPushMessage(gimbal_pub, (void *)&gimbal_feedback_data);
|
PubPushMessage(gimbal_pub, (void *)&gimbal_feedback_data);
|
||||||
}
|
}
|
||||||
@@ -26,7 +26,7 @@
|
|||||||
|
|
||||||
/* 机器人重要参数定义,注意根据不同机器人进行修改,浮点数需要以.0或f结尾,无符号以u结尾 */
|
/* 机器人重要参数定义,注意根据不同机器人进行修改,浮点数需要以.0或f结尾,无符号以u结尾 */
|
||||||
// 云台参数
|
// 云台参数
|
||||||
#define YAW_CHASSIS_ALIGN_ECD 8015 // 云台和底盘对齐指向相同方向时的电机编码器值,若对云台有机械改动需要修改
|
#define YAW_CHASSIS_ALIGN_ECD 3938 // 云台和底盘对齐指向相同方向时的电机编码器值,若对云台有机械改动需要修改
|
||||||
#define YAW_ECD_GREATER_THAN_4096 0 // ALIGN_ECD值是否大于4096,是为1,否为0;用于计算云台偏转角度
|
#define YAW_ECD_GREATER_THAN_4096 0 // ALIGN_ECD值是否大于4096,是为1,否为0;用于计算云台偏转角度
|
||||||
#define PITCH_HORIZON_ECD 3412 // 云台处于水平位置时编码器值,若对云台有机械改动需要修改
|
#define PITCH_HORIZON_ECD 3412 // 云台处于水平位置时编码器值,若对云台有机械改动需要修改
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||||||
#define PITCH_MAX_ANGLE 0 // 云台竖直方向最大角度 (注意反馈如果是陀螺仪,则填写陀螺仪的角度)
|
#define PITCH_MAX_ANGLE 0 // 云台竖直方向最大角度 (注意反馈如果是陀螺仪,则填写陀螺仪的角度)
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||||||
@@ -35,11 +35,11 @@
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|||||||
// #define CHASSIS_OMNI_WHEEL // 是否为全向轮底盘
|
// #define CHASSIS_OMNI_WHEEL // 是否为全向轮底盘
|
||||||
// #define CHASSIS_MCNAMEE_WHEEL // 是否为麦克纳姆轮底盘
|
// #define CHASSIS_MCNAMEE_WHEEL // 是否为麦克纳姆轮底盘
|
||||||
#define CHASSIS_STEERING_WHEEL // 是否为舵轮
|
#define CHASSIS_STEERING_WHEEL // 是否为舵轮
|
||||||
#define STEERING_CHASSIS_ALIGN_ECD_LF 7367 // 舵电机 A 编码器值,若有机械改动需要修改
|
#define STEERING_CHASSIS_ALIGN_ECD_RF 7367 // 舵电机 A 编码器值,若有机械改动需要修改
|
||||||
#define STEERING_CHASSIS_ALIGN_ECD_RB 1195 // 舵电机 D 编码器值,若有机械改动需要修改
|
#define STEERING_CHASSIS_ALIGN_ECD_LB 1195 // 舵电机 D 编码器值,若有机械改动需要修改
|
||||||
|
|
||||||
#define STEERING_CHASSIS_ALIGN_ANGLE_LF STEERING_CHASSIS_ALIGN_ECD_LF / 8192.f * 360.f // 舵轮 A 对齐角度
|
#define STEERING_CHASSIS_ALIGN_ANGLE_RF STEERING_CHASSIS_ALIGN_ECD_RF / 8192.f * 360.f // 舵轮 A 对齐角度
|
||||||
#define STEERING_CHASSIS_ALIGN_ANGLE_RB STEERING_CHASSIS_ALIGN_ECD_RB / 8192.f * 360.f // 舵轮 D 对齐角度
|
#define STEERING_CHASSIS_ALIGN_ANGLE_LB STEERING_CHASSIS_ALIGN_ECD_LB / 8192.f * 360.f // 舵轮 D 对齐角度
|
||||||
// 发射参数
|
// 发射参数
|
||||||
#define ONE_BULLET_DELTA_ANGLE 36 // 发射一发弹丸拨盘转动的距离,由机械设计图纸给出
|
#define ONE_BULLET_DELTA_ANGLE 36 // 发射一发弹丸拨盘转动的距离,由机械设计图纸给出
|
||||||
#define REDUCTION_RATIO_LOADER 49.0f // 拨盘电机的减速比,英雄需要修改为3508的19.0f
|
#define REDUCTION_RATIO_LOADER 49.0f // 拨盘电机的减速比,英雄需要修改为3508的19.0f
|
||||||
@@ -207,7 +207,7 @@ typedef struct
|
|||||||
{
|
{
|
||||||
attitude_t gimbal_imu_data;
|
attitude_t gimbal_imu_data;
|
||||||
uint16_t yaw_motor_single_round_angle;
|
uint16_t yaw_motor_single_round_angle;
|
||||||
float yaw_motor_total_angle;
|
uint16_t yaw_motor_total_angle;
|
||||||
} Gimbal_Upload_Data_s;
|
} Gimbal_Upload_Data_s;
|
||||||
|
|
||||||
typedef struct
|
typedef struct
|
||||||
|
|||||||
@@ -96,7 +96,7 @@ void ShootInit()
|
|||||||
.close_loop_type = CURRENT_LOOP | SPEED_LOOP,
|
.close_loop_type = CURRENT_LOOP | SPEED_LOOP,
|
||||||
.motor_reverse_flag = MOTOR_DIRECTION_NORMAL, // 注意方向设置为拨盘的拨出的击发方向
|
.motor_reverse_flag = MOTOR_DIRECTION_NORMAL, // 注意方向设置为拨盘的拨出的击发方向
|
||||||
},
|
},
|
||||||
.motor_type = M2006 // 英雄使用m3508
|
.motor_type = M3508 // 英雄使用m3508
|
||||||
};
|
};
|
||||||
loader = DJIMotorInit(&loader_config);
|
loader = DJIMotorInit(&loader_config);
|
||||||
|
|
||||||
|
|||||||
@@ -28,6 +28,6 @@ void LEDSet(LEDInstance *_led,uint8_t alpha,uint8_t color_value,uint8_t brightne
|
|||||||
|
|
||||||
void LEDSwitch(LEDInstance *_led,uint8_t led_switch);
|
void LEDSwitch(LEDInstance *_led,uint8_t led_switch);
|
||||||
|
|
||||||
void LEDShow();
|
void LEDShow(uint32_t aRGB);
|
||||||
|
|
||||||
#endif // !_LED_H_
|
#endif // !_LED_H_
|
||||||
|
|||||||
@@ -40,7 +40,7 @@ static void sbus_to_rc(const uint8_t *sbus_buf)
|
|||||||
rc_ctrl[TEMP].rc.rocker_l_ = (((sbus_buf[2] >> 6) | (sbus_buf[3] << 2) | (sbus_buf[4] << 10)) & 0x07ff) - RC_CH_VALUE_OFFSET; //!< Channel 2
|
rc_ctrl[TEMP].rc.rocker_l_ = (((sbus_buf[2] >> 6) | (sbus_buf[3] << 2) | (sbus_buf[4] << 10)) & 0x07ff) - RC_CH_VALUE_OFFSET; //!< Channel 2
|
||||||
rc_ctrl[TEMP].rc.rocker_l1 = (((sbus_buf[4] >> 1) | (sbus_buf[5] << 7)) & 0x07ff) - RC_CH_VALUE_OFFSET; //!< Channel 3
|
rc_ctrl[TEMP].rc.rocker_l1 = (((sbus_buf[4] >> 1) | (sbus_buf[5] << 7)) & 0x07ff) - RC_CH_VALUE_OFFSET; //!< Channel 3
|
||||||
rc_ctrl[TEMP].rc.dial = ((sbus_buf[16] | (sbus_buf[17] << 8)) & 0x07FF) - RC_CH_VALUE_OFFSET;
|
rc_ctrl[TEMP].rc.dial = ((sbus_buf[16] | (sbus_buf[17] << 8)) & 0x07FF) - RC_CH_VALUE_OFFSET;
|
||||||
rc_ctrl[TEMP].rc.rocker_l_= rc_ctrl[TEMP].rc.rocker_l_+3;
|
rc_ctrl[TEMP].rc.rocker_l_= rc_ctrl[TEMP].rc.rocker_l_;
|
||||||
// 左侧拨轮
|
// 左侧拨轮
|
||||||
RectifyRCjoystick();
|
RectifyRCjoystick();
|
||||||
// 开关,0左1右
|
// 开关,0左1右
|
||||||
|
|||||||
Reference in New Issue
Block a user