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https://gitee.com/dlmu-cone/half-steering-basic-framework
synced 2026-10-24 01:52:20 +08:00
6020pitch driver
This commit is contained in:
@@ -207,6 +207,10 @@ static void RemoteControlSet()
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gimbal_cmd_send.pitch += 0.001f * (float)rc_data[TEMP].rc.rocker_l1;
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gimbal_cmd_send.pitch += 0.001f * (float)rc_data[TEMP].rc.rocker_l1;
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}
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}
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// 云台软件限位
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// 云台软件限位
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if (gimbal_cmd_send.pitch > PITCH_MAX_ANGLE)
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gimbal_cmd_send.pitch = PITCH_MAX_ANGLE;
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else if (gimbal_cmd_send.pitch < PITCH_MIN_ANGLE)
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gimbal_cmd_send.pitch = PITCH_MIN_ANGLE;
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// 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
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// 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
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chassis_cmd_send.vx = 0.15f * (float)rc_data[TEMP].rc.rocker_r_; // _水平方向
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chassis_cmd_send.vx = 0.15f * (float)rc_data[TEMP].rc.rocker_r_; // _水平方向
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@@ -244,6 +248,12 @@ static void MouseKeySet()
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gimbal_cmd_send.yaw += (float)rc_data[TEMP].mouse.x / 660 * 10; // 系数待测
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gimbal_cmd_send.yaw += (float)rc_data[TEMP].mouse.x / 660 * 10; // 系数待测
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gimbal_cmd_send.pitch += (float)rc_data[TEMP].mouse.y / 660 * 10;
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gimbal_cmd_send.pitch += (float)rc_data[TEMP].mouse.y / 660 * 10;
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// 云台软件限位
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if (gimbal_cmd_send.pitch > PITCH_MAX_ANGLE)
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gimbal_cmd_send.pitch = PITCH_MAX_ANGLE;
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else if (gimbal_cmd_send.pitch < PITCH_MIN_ANGLE)
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gimbal_cmd_send.pitch = PITCH_MIN_ANGLE;
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switch (rc_data[TEMP].key_count[KEY_PRESS][Key_Z] % 3) // Z键设置弹速
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switch (rc_data[TEMP].key_count[KEY_PRESS][Key_Z] % 3) // Z键设置弹速
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{
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{
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case 0:
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case 0:
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@@ -66,24 +66,20 @@ void GimbalInit()
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Motor_Init_Config_s pitch_config = {
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Motor_Init_Config_s pitch_config = {
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.can_init_config = {
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.can_init_config = {
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.can_handle = &hcan2,
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.can_handle = &hcan2,
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.tx_id = 4,//2
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.tx_id = 2,//2
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},
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},
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.controller_param_init_config = {
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.controller_param_init_config = {
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.angle_PID = {
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.angle_PID = {
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.Kp = 10, // 10
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.Kp = 40, // 10
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.Ki = 0,
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.Ki = 0,
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.Kd = 0,
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.Kd = 0,
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.Improve = PID_Trapezoid_Intergral | PID_Integral_Limit | PID_Derivative_On_Measurement,
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.MaxOut = 1000,
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.IntegralLimit = 100,
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.MaxOut = 500,
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},
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},
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.speed_PID = {
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.speed_PID = {
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.Kp = 50, // 50
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.Kp = 80, // 50
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.Ki = 350, // 350
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.Ki = 15, // 350
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.Kd = 0, // 0
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.Kd = 0.6, // 0
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.Improve = PID_Trapezoid_Intergral | PID_Integral_Limit | PID_Derivative_On_Measurement,
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.MaxOut = 30000,//20000
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.IntegralLimit = 2500,
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.MaxOut = 8000,//20000
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},
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},
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.other_angle_feedback_ptr = &gimba_IMU_data->Pitch,
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.other_angle_feedback_ptr = &gimba_IMU_data->Pitch,
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// 还需要增加角速度额外反馈指针,注意方向,ins_task.md中有c板的bodyframe坐标系说明
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// 还需要增加角速度额外反馈指针,注意方向,ins_task.md中有c板的bodyframe坐标系说明
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@@ -94,9 +90,11 @@ void GimbalInit()
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.speed_feedback_source = OTHER_FEED,
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.speed_feedback_source = OTHER_FEED,
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.outer_loop_type = ANGLE_LOOP,
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.outer_loop_type = ANGLE_LOOP,
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.close_loop_type = SPEED_LOOP | ANGLE_LOOP,
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.close_loop_type = SPEED_LOOP | ANGLE_LOOP,
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// .outer_loop_type = SPEED_LOOP,//调试用
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// .close_loop_type = SPEED_LOOP,
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.motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
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.motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
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},
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},
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.motor_type = DM4310,
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.motor_type = GM6020,
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};
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};
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// 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
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// 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
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yaw_motor = DJIMotorInit(&yaw_config);
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yaw_motor = DJIMotorInit(&yaw_config);
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@@ -29,8 +29,8 @@
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#define YAW_CHASSIS_ALIGN_ECD 1190 // 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
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#define YAW_CHASSIS_ALIGN_ECD 1190 // 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
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#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
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#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
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#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_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)
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#define PITCH_MAX_ANGLE 30 // 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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#define PITCH_MIN_ANGLE 0 // 云台竖直方向最小角度 (注意反馈如果是陀螺仪,则填写陀螺仪的角度)
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#define PITCH_MIN_ANGLE -20 // 云台竖直方向最小角度 (注意反馈如果是陀螺仪,则填写陀螺仪的角度)
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// 底盘参数
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// 底盘参数
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// #define CHASSIS_OMNI_WHEEL // 是否为全向轮底盘
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// #define CHASSIS_OMNI_WHEEL // 是否为全向轮底盘
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// #define CHASSIS_MCNAMEE_WHEEL // 是否为麦克纳姆轮底盘
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// #define CHASSIS_MCNAMEE_WHEEL // 是否为麦克纳姆轮底盘
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@@ -42,7 +42,7 @@
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#define STEERING_CHASSIS_ALIGN_ANGLE_LB STEERING_CHASSIS_ALIGN_ECD_LB / 8192.f * 360.f // 舵轮 D 对齐角度
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#define STEERING_CHASSIS_ALIGN_ANGLE_LB STEERING_CHASSIS_ALIGN_ECD_LB / 8192.f * 360.f // 舵轮 D 对齐角度
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// 发射参数
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// 发射参数
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#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
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#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
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#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
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#define REDUCTION_RATIO_LOADER 36.0f // 拨盘电机的减速比,英雄需要修改为3508的19.0f
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#define NUM_PER_CIRCLE 10 // 拨盘一圈的装载量
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#define NUM_PER_CIRCLE 10 // 拨盘一圈的装载量
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// 机器人底盘修改的参数,单位为mm(毫米)
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// 机器人底盘修改的参数,单位为mm(毫米)
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#define WHEEL_BASE 350 // 纵向轴距(前进后退方向)
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#define WHEEL_BASE 350 // 纵向轴距(前进后退方向)
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@@ -52,10 +52,10 @@ void ShootInit()
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.motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
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.motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
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},
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},
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.motor_type = M3508};
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.motor_type = M3508};
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friction_config.can_init_config.tx_id = 1,
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friction_config.can_init_config.tx_id = 3,
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friction_l = DJIMotorInit(&friction_config);
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friction_l = DJIMotorInit(&friction_config);
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friction_config.can_init_config.tx_id = 2; // 右摩擦轮,改txid和方向就行
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friction_config.can_init_config.tx_id = 4; // 右摩擦轮,改txid和方向就行
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friction_config.controller_setting_init_config.motor_reverse_flag = MOTOR_DIRECTION_REVERSE;
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friction_config.controller_setting_init_config.motor_reverse_flag = MOTOR_DIRECTION_REVERSE;
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friction_r = DJIMotorInit(&friction_config);
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friction_r = DJIMotorInit(&friction_config);
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@@ -199,8 +199,8 @@ void IMU_QuaternionEKF_Update(float gx, float gy, float gz, float ax, float ay,
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// 利用四元数反解欧拉角
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// 利用四元数反解欧拉角
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QEKF_INS.Yaw = atan2f(2.0f * (QEKF_INS.q[0] * QEKF_INS.q[3] + QEKF_INS.q[1] * QEKF_INS.q[2]), 2.0f * (QEKF_INS.q[0] * QEKF_INS.q[0] + QEKF_INS.q[1] * QEKF_INS.q[1]) - 1.0f) * 57.295779513f;
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QEKF_INS.Yaw = atan2f(2.0f * (QEKF_INS.q[0] * QEKF_INS.q[3] + QEKF_INS.q[1] * QEKF_INS.q[2]), 2.0f * (QEKF_INS.q[0] * QEKF_INS.q[0] + QEKF_INS.q[1] * QEKF_INS.q[1]) - 1.0f) * 57.295779513f;
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QEKF_INS.Pitch = atan2f(2.0f * (QEKF_INS.q[0] * QEKF_INS.q[1] + QEKF_INS.q[2] * QEKF_INS.q[3]), 2.0f * (QEKF_INS.q[0] * QEKF_INS.q[0] + QEKF_INS.q[3] * QEKF_INS.q[3]) - 1.0f) * 57.295779513f;
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QEKF_INS.Pitch = -asinf(-2.0f * (QEKF_INS.q[1] * QEKF_INS.q[3] - QEKF_INS.q[0] * QEKF_INS.q[2])) * 57.295779513f;
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QEKF_INS.Roll = asinf(-2.0f * (QEKF_INS.q[1] * QEKF_INS.q[3] - QEKF_INS.q[0] * QEKF_INS.q[2])) * 57.295779513f;
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QEKF_INS.Roll = atan2f(2.0f * (QEKF_INS.q[0] * QEKF_INS.q[1] + QEKF_INS.q[2] * QEKF_INS.q[3]), 2.0f * (QEKF_INS.q[0] * QEKF_INS.q[0] + QEKF_INS.q[3] * QEKF_INS.q[3]) - 1.0f) * 57.295779513f;
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// get Yaw total, yaw数据可能会超过360,处理一下方便其他功能使用(如小陀螺)
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// get Yaw total, yaw数据可能会超过360,处理一下方便其他功能使用(如小陀螺)
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if (QEKF_INS.Yaw - QEKF_INS.YawAngleLast > 180.0f)
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if (QEKF_INS.Yaw - QEKF_INS.YawAngleLast > 180.0f)
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@@ -24,7 +24,7 @@ static CANInstance sender_assignment[6] = {
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[1] = {.can_handle = &hcan1, .txconf.StdId = 0x200, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[1] = {.can_handle = &hcan1, .txconf.StdId = 0x200, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[2] = {.can_handle = &hcan1, .txconf.StdId = 0x2ff, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[2] = {.can_handle = &hcan1, .txconf.StdId = 0x2ff, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[3] = {.can_handle = &hcan2, .txconf.StdId = 0x1ff, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[3] = {.can_handle = &hcan2, .txconf.StdId = 0x1ff, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[4] = {.can_handle = &hcan2, .txconf.StdId = 0x3FE, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[4] = {.can_handle = &hcan2, .txconf.StdId = 0x200, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[5] = {.can_handle = &hcan2, .txconf.StdId = 0x2ff, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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[5] = {.can_handle = &hcan2, .txconf.StdId = 0x2ff, .txconf.IDE = CAN_ID_STD, .txconf.RTR = CAN_RTR_DATA, .txconf.DLC = 0x08, .tx_buff = {0}},
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};
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};
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@@ -321,25 +321,15 @@ void DJIMotorControl()
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// 获取最终输出
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// 获取最终输出
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set = (int16_t)pid_ref;
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set = (int16_t)pid_ref;
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// 分组填入发送数据
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// 分组填入发送数据
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group = motor->sender_group;
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group = motor->sender_group;
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num = motor->message_num;
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num = motor->message_num;
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if (i == 1)
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{
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sender_assignment[4].tx_buff[6] = (uint8_t)(set & 0x00ff); // 高八位
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sender_assignment[4].tx_buff[7] = (uint8_t)(set >> 8); // 低八位
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}
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else
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{
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sender_assignment[group].tx_buff[2 * num] = (uint8_t)(set >> 8); // 低八位
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sender_assignment[group].tx_buff[2 * num] = (uint8_t)(set >> 8); // 低八位
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sender_assignment[group].tx_buff[2 * num + 1] = (uint8_t)(set & 0x00ff); // 高八位
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sender_assignment[group].tx_buff[2 * num + 1] = (uint8_t)(set & 0x00ff); // 高八位
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}
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// 若该电机处于停止状态,直接将buff置零
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// 若该电机处于停止状态,直接将buff置零
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if (motor->stop_flag == MOTOR_STOP)
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if (motor->stop_flag == MOTOR_STOP)
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memset(sender_assignment[group].tx_buff + 2 * num, 0, 2u);
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memset(sender_assignment[group].tx_buff + 2 * num, 0, sizeof(uint16_t));
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}
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}
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// 遍历flag,检查是否要发送这一帧报文
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// 遍历flag,检查是否要发送这一帧报文
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