421 lines
18 KiB
C
421 lines
18 KiB
C
#include "Chassis.h"
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#include "define.h"
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/*舵轮舵向校准方法：注释掉关于6020反馈角度的处理以及6020数据的发送这两处，
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进debug将四个轮子编码器朝右（左右无所谓，可能会导致5065方向反，在解算里加个负号就行）
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查看6020反馈值，将6020反馈值放入motor_offset中*/
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//底盘初始化
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int8_t Chassis_init(Chassis_t *c,const Chassis_Param_t *param,float target_freq){
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c->param = param; /*初始化参数 */
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//舵轮安装时的6020机械误差，机械校准时1号轮在左前方，所有轮的编码器朝向右面
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MotorOffset_t motor_offset = { {30.303986, 149.937744, 268.077156, 29.820541}};
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c->motoroffset = motor_offset; // 将 motor_offset 的值赋给 c->motoroffset
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//在这里修改雷达校准时sick的值 (标号为逆时针)
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c->SICK_FALG = 0;
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c->sick_set[0] = 2500;
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c->sick_set[1] = 2500;
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c->sick_set[2] = 600;
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//蜂鸣器初始化
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Buzzer_Init(&c->buzzer_radar_angle,200,1000,0.5);
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Buzzer_Init(&c->buzzer_sick_calibration,200,1000,0.5);
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PID_init(&(c->pid.chassis_6020OmegaPid), PID_POSITION,&(c->param->C6020Omega_param));
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PID_init(&(c->pid.chassis_6020anglePid), PID_POSITION,&(c->param->C6020Angle_param));
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PID_init(&(c->pid.chassis_RadaranglePID),PID_POSITION,&(c->param->RadarAngle_param));
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PID_init(&(c->pid.chassis_RadarspeedPID),PID_POSITION,&(c->param->RadarSpeed_param));
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PID_init(&(c->pid.chassis_SickVx), PID_POSITION,&(c->param->SickVx_param));
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PID_init(&(c->pid.chassis_SickVy), PID_POSITION,&(c->param->SickVy_param));
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PID_init(&(c->pid.chassis_SickVw), PID_POSITION,&(c->param->SickVw_param));
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LowPassFilter2p_Init(&(c->filled[0]),target_freq,80.0f); //给x 做滤波
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LowPassFilter2p_Init(&(c->filled[1]),target_freq,80.0f); //给y 做滤波
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LowPassFilter2p_Init(&(c->filled[2]),target_freq,80.0f); //给w 做滤波
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LowPassFilter2p_Init(&(c->filled[3]),target_freq,8.0f); //给雷达x做滤波
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LowPassFilter2p_Init(&(c->filled[4]),target_freq,8.0f); //给雷达y做滤波
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LowPassFilter2p_Init(&(c->filled[5]),target_freq,8.0f); //给雷达z做滤波
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LowPassFilter2p_Init(&(c->filled[6]),target_freq,10.0f); //给sick1做滤波
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LowPassFilter2p_Init(&(c->filled[7]),target_freq,10.0f); //给sick2做滤波
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LowPassFilter2p_Init(&(c->filled[8]),target_freq,10.0f); //给sick3做滤波
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return CHASSIS_OK;
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}
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static int8_t Chassis_SetCtrl(Chassis_t *c,CMD_t *ctrl){
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c->mode =ctrl->C_cmd.mode;
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c->pos =ctrl->C_cmd.pos;
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return 0;
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}
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//该函数用来更新其他任务获得的数据
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int8_t Chassis_UpdateFeedback(Chassis_t *c, const CAN_t *can) {
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for (uint8_t i = 0; i < 4; i++) {
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c->motorfeedback.rotor_rpm3508[i] = can->motor.motor3508.as_array[i].rotor_speed;
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c->motorfeedback.rotor_current3508[i] = can->motor.motor3508.as_array[i].torque_current;
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c->motorfeedback.rotor_rpm6020[i] = can->motor.chassis6020.as_array[i].rotor_speed;
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c->motorfeedback.rotor_current6020[i] = can->motor.chassis6020.as_array[i].torque_current;
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c->motorfeedback.rotor_angle6020[i] = can->motor.chassis6020.as_array[i].rotor_angle;
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c->motorfeedback.rotor_temp6020[i] = can->motor.chassis6020.as_array[i].temp;
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#ifdef calibration
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#else
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//由于安装不能保证0点朝向我们想要朝向的方向，所以进行零点偏移
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c->motorfeedback.rotor_angle6020[i] = fmod(can->motor.chassis6020.as_array[i].rotor_angle -
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c->motoroffset.MOTOR_OFFSET[i], 360.0);
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if(c->motorfeedback.rotor_angle6020[i]<0){
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c->motorfeedback.rotor_angle6020[i]+=360;
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}
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#endif
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c->motorfeedback.rotor_rpm5065[i] = can->motor.chassis5065.as_array[i].rotor_speed;
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c->motorfeedback.torque_current5065[i] = can->motor.chassis5065.as_array[i].torque_current;
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}
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//接收sick数据
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for (uint8_t i = 0; i < 3; i++) {
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c->sick[i] = can->sickfed.as_array[i].sick_distance/10;
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}
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return CHASSIS_OK;
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}
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//底盘解算
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void Chassis_speed_calculate(Chassis_t *c,Action_POS_t*pos) {
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// RC模式下松开遥控器防止6020回到默认位置导致侧翻
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if (c->mode == RC&&fabs(c->move_vec.Vx) < 3000 && fabs(c->move_vec.Vy) < 3000 && fabs(c->move_vec.Vw) < 3000) {
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// 如果之前不处于保持模式，则记录当前角度
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if (!c->keeping_angle_flag) {
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c->keeping_angle_flag = 1; // 进入保持模式
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}
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// 使用保持的角度，而不是实时反馈值,速度为0
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for (uint8_t i = 0; i < 4; i++) {
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c->hopemotorout.rotor6020_jiesuan_1[i] = c->keep_angle[i];
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c->hopemotorout.rotor5065_jiesuan_1[i] = 0;
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}
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}
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else {
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// 如果有速度输入，则退出保持模式
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c->keeping_angle_flag = 0;
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//让保持角度实时等于进入保持阈值前的最后一次角度值
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for (uint8_t i = 0; i < 4; i++) {
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c->keep_angle[i] = c->hopemotorout.rotor6020_jiesuan_1[i];
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}
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switch(c->mode){
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case RC: //RC模式下遥控器控制底盘运动，操控为机器人坐标系 x朝前，y朝右
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//解算得到5065速度，加-号是因为vesc校准时轮向电机默认转动正方向不同，可从上位机里改
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c->hopemotorout.rotor5065_jiesuan_1[0]=-sqrt(
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians))*(c->move_vec.Vx+c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy+c->move_vec.Vw*cos(radians))*(c->move_vec.Vy+c->move_vec.Vw*cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[1]=sqrt(
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians))*(c->move_vec.Vx-c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy+c->move_vec.Vw*cos(radians))*(c->move_vec.Vy+c->move_vec.Vw*cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[2]=-sqrt(
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians))*(c->move_vec.Vx+c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy-c->move_vec.Vw*cos(radians))*(c->move_vec.Vy-c->move_vec.Vw*cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[3]=sqrt(
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians))*(c->move_vec.Vx-c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy-c->move_vec.Vw*cos(radians))*(c->move_vec.Vy-c->move_vec.Vw*cos(radians)));
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//解算得到6020角度（-180°——+180°）
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c->hopemotorout.rotor6020_jiesuan_1[0]=atan2((c->move_vec.Vy+c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[1]=atan2((c->move_vec.Vy+c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[2]=atan2((c->move_vec.Vy-c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[3]=atan2((c->move_vec.Vy-c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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break;
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case STOP: //停止模式下轮子锁死
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for(int i =0 ; i < 4 ; i++){
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c->hopemotorout.rotor5065_jiesuan_1[i]=0;
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}
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c->hopemotorout.rotor6020_jiesuan_1[0]=315;
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c->hopemotorout.rotor6020_jiesuan_1[1]=45;
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c->hopemotorout.rotor6020_jiesuan_1[2]=45;
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c->hopemotorout.rotor6020_jiesuan_1[3]=315;
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break;
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case NAVI:
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#ifdef radar
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//相机，雷达纠正时就用正常解算
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c->hopemotorout.rotor5065_jiesuan_1[0]=-sqrt(
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians))*(c->move_vec.Vx+c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy+c->move_vec.Vw*cos(radians))*(c->move_vec.Vy+c->move_vec.Vw*cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[1]=sqrt(
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians))*(c->move_vec.Vx-c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy+c->move_vec.Vw*cos(radians))*(c->move_vec.Vy+c->move_vec.Vw*cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[2]=-sqrt(
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians))*(c->move_vec.Vx+c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy-c->move_vec.Vw*cos(radians))*(c->move_vec.Vy-c->move_vec.Vw*cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[3]=sqrt(
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians))*(c->move_vec.Vx-c->move_vec.Vw*sin(radians))+
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(c->move_vec.Vy-c->move_vec.Vw*cos(radians))*(c->move_vec.Vy-c->move_vec.Vw*cos(radians)));
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//解算得到6020角度（-180°——+180°）
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c->hopemotorout.rotor6020_jiesuan_1[0]=atan2((c->move_vec.Vy+c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[1]=atan2((c->move_vec.Vy+c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[2]=atan2((c->move_vec.Vy-c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx+c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[3]=atan2((c->move_vec.Vy-c->move_vec.Vw*cos(radians)),
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(c->move_vec.Vx-c->move_vec.Vw*sin(radians)))* (180 / M_PI);
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#elif defined(action_sick)
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//码盘sick模式下操控为世界坐标系，能实现舵轮小陀螺前进
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c->chassis_yaw = pos->pos_yaw* (M_PI / 180.0f);
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float cos_yaw = cosf(c->chassis_yaw);
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float sin_yaw = sinf(c->chassis_yaw);
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// 将速度从世界坐标系转换到底盘坐标系
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float Vx_local = c->move_vec.Vx * cos_yaw + c->move_vec.Vy * sin_yaw;
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float Vy_local = -c->move_vec.Vx * sin_yaw + c->move_vec.Vy * cos_yaw;
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//解算得到5065速度，加-号是因为vesc校准时轮向电机默认转动正方向不同，可从上位机里改
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c->hopemotorout.rotor5065_jiesuan_1[0]=-sqrt(
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(Vx_local + c->move_vec.Vw * sin(radians)) * (Vx_local + c->move_vec.Vw * sin(radians)) +
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(Vy_local + c->move_vec.Vw * cos(radians)) * (Vy_local + c->move_vec.Vw * cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[1]=sqrt(
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(Vx_local - c->move_vec.Vw * sin(radians)) * (Vx_local - c->move_vec.Vw * sin(radians)) +
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(Vy_local + c->move_vec.Vw * cos(radians)) * (Vy_local + c->move_vec.Vw * cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[2]=-sqrt(
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(Vx_local + c->move_vec.Vw * sin(radians)) * (Vx_local + c->move_vec.Vw * sin(radians)) +
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(Vy_local - c->move_vec.Vw * cos(radians)) * (Vy_local - c->move_vec.Vw * cos(radians)));
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c->hopemotorout.rotor5065_jiesuan_1[3]=sqrt(
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(Vx_local - c->move_vec.Vw * sin(radians)) * (Vx_local - c->move_vec.Vw * sin(radians)) +
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(Vy_local - c->move_vec.Vw * cos(radians)) * (Vy_local - c->move_vec.Vw * cos(radians)));
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//解算得到6020角度（-180°——+180°）
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c->hopemotorout.rotor6020_jiesuan_1[0]= atan2((Vy_local + c->move_vec.Vw * cos(radians)),
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(Vx_local + c->move_vec.Vw * sin(radians))) * (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[1]= atan2((Vy_local + c->move_vec.Vw * cos(radians)),
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(Vx_local - c->move_vec.Vw * sin(radians))) * (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[2]= atan2((Vy_local - c->move_vec.Vw * cos(radians)),
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(Vx_local + c->move_vec.Vw * sin(radians))) * (180 / M_PI);
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c->hopemotorout.rotor6020_jiesuan_1[3]= atan2((Vy_local - c->move_vec.Vw * cos(radians)),
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(Vx_local - c->move_vec.Vw * sin(radians))) * (180 / M_PI);
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#endif
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break;
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}
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}
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//角度归化到0°——360°
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for (uint8_t i = 0; i < 4; i++) {
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if(c->hopemotorout.rotor6020_jiesuan_1[i]<0){
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c->hopemotorout.rotor6020_jiesuan_1[i]+=360;
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}
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}
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//舵向电机就近转位
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float angle_error[4];//角度误差
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for (uint8_t i = 0; i < 4; i++) {
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angle_error[i]=c->hopemotorout.rotor6020_jiesuan_1[i]-c->motorfeedback.rotor_angle6020[i];
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//误差角度归化到-180°——+180°
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while (angle_error[i] > 180) angle_error[i] -= 360;
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while (angle_error[i] < -180) angle_error[i] += 360;
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/*这里发现如果下面的c->motorfeedback.rotor_angle6020[i]+angle_error[i]变为
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c->hopemotorout.rotor6020_jiesuan_1[i]会导致6020出现故障*/
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if(angle_error[i]>90&&angle_error[i]<=180){
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c->hopemotorout.rotor5065_jiesuan_2[i]=-c->hopemotorout.rotor5065_jiesuan_1[i];
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c->hopemotorout.rotor6020_jiesuan_2[i]=c->motorfeedback.rotor_angle6020[i]+angle_error[i]-180;
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}
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else if(angle_error[i]<-90&&angle_error[i]>=-180){
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c->hopemotorout.rotor5065_jiesuan_2[i]=-c->hopemotorout.rotor5065_jiesuan_1[i];
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c->hopemotorout.rotor6020_jiesuan_2[i]=c->motorfeedback.rotor_angle6020[i]+angle_error[i]+180;
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}
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else{
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c->hopemotorout.rotor5065_jiesuan_2[i]=c->hopemotorout.rotor5065_jiesuan_1[i];
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c->hopemotorout.rotor6020_jiesuan_2[i]=c->motorfeedback.rotor_angle6020[i]+angle_error[i];
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}
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}
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}
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//nuc纠正角度（右旋偏移量为正，左旋偏移量为负）
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void nuc_angle_correct(Chassis_t *c,CMD_t *ctrl){
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//双环pid
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// fp32 nuc_detangle;
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// nuc_detangle = - PID_calc(&(c->pid.chassis_RadaranglePID),ctrl->nuc.vw,0);
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// c->radar_yaw = PID_calc(&(c->pid.chassis_RadarspeedPID),c->pos088.bmi088.gyro.z,nuc_detangle);
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//两个单环pid
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if(fabsf(ctrl->nuc.vw)>8){
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c->radar_yaw = - PID_calc(&(c->pid.chassis_RadaranglePID),ctrl->nuc.vw,0)*8;
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}
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else{
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c->radar_yaw = - PID_calc(&(c->pid.chassis_RadarspeedPID),ctrl->nuc.vw,0)*20;
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}
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}
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//雷达运用sick来校准
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void radar_sick_calibration(Chassis_t *c){
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fp32 diff_x = c->sick[2] - c->sick_set[2];
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fp32 diff_y = c->sick[0] - c->sick_set[0];
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fp32 diff_w = (c->sick[0] - c->sick[1]); //放大偏角误差
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c->move_sick.Vx = (fabsf(diff_x)>SICKXY_ERROR) ? PID_calc(&(c->pid.chassis_SickVx),diff_x,0): 0;
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c->move_sick.Vy = (fabsf(diff_y)>SICKXY_ERROR) ? PID_calc(&(c->pid.chassis_SickVy),diff_y,0): 0;
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c->move_sick.Vw = (fabsf(diff_w)>SICKW_ERROR) ? PID_calc(&(c->pid.chassis_SickVw),diff_w*4,0): 0;
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//判断sick是否到达目标点附近
|
||
static uint8_t reach_cnt = 0;
|
||
if (fabsf(diff_x) <= SICKXY_ERROR && fabsf(diff_y) <= SICKXY_ERROR &&fabsf(diff_w)<= SICKW_ERROR) {
|
||
reach_cnt++;
|
||
if (reach_cnt >= 50) {
|
||
c->SICK_FALG = 1;
|
||
reach_cnt = 0;
|
||
}
|
||
}
|
||
else {
|
||
c->SICK_FALG = 0;
|
||
}
|
||
|
||
//由于r1到达sick目标点附近可能会震荡，所以必须是锁死时到达目标点才给nuc发数
|
||
if(c->SICK_FALG == 1 && c->mode ==STOP){
|
||
c->SICK__SEND_FALG = 1;
|
||
}
|
||
else {
|
||
c->SICK__SEND_FALG = 0;
|
||
}
|
||
}
|
||
|
||
//底盘控制
|
||
int8_t Chassis_Control(Chassis_t *c,CMD_t *ctrl,CAN_Output_t *out, Action_POS_t*pos){
|
||
|
||
Chassis_SetCtrl(c,ctrl);
|
||
|
||
fp32 chassis6020_detangle[4];
|
||
|
||
#ifdef radar
|
||
//关于nuc纠正的函数都要一直运行
|
||
|
||
//雷达数据必须滤波，否则波形是0和正常数组成的矩形
|
||
ctrl->nuc.vx = LowPassFilter2p_Apply(&(c->filled[3]),ctrl->nuc.vx);
|
||
ctrl->nuc.vy = LowPassFilter2p_Apply(&(c->filled[4]),ctrl->nuc.vy);
|
||
ctrl->nuc.vw = LowPassFilter2p_Apply(&(c->filled[5]),ctrl->nuc.vw);
|
||
|
||
c->sick[0] = LowPassFilter2p_Apply(&(c->filled[6]),c->sick[0]);
|
||
c->sick[1] = LowPassFilter2p_Apply(&(c->filled[7]),c->sick[1]);
|
||
c->sick[2] = LowPassFilter2p_Apply(&(c->filled[8]),c->sick[2]);
|
||
|
||
nuc_angle_correct(c,ctrl);
|
||
radar_sick_calibration(c);
|
||
#endif
|
||
switch (c->mode){
|
||
case RC:
|
||
c->move_vec.Vx = ctrl->Vx*ctrl->throttle*9500;
|
||
c->move_vec.Vy = ctrl->Vy*ctrl->throttle*9500;
|
||
c->move_vec.Vw = ctrl->Vw*ctrl->throttle*6000;
|
||
|
||
break;
|
||
|
||
case STOP:
|
||
c->move_vec.Vx =0;
|
||
c->move_vec.Vy =0;
|
||
c->move_vec.Vw =0;
|
||
Buzzer_Control(&c->buzzer_sick_calibration,(c->SICK_FALG == 1));
|
||
Buzzer_Control(&c->buzzer_radar_angle,(fabsf(ctrl->nuc.vw) < 1 && ctrl->nuc.vw != 0));
|
||
break;
|
||
|
||
case NAVI:
|
||
#ifdef radar
|
||
switch (ctrl->C_cmd.nuc_radar){
|
||
case ANGLE:
|
||
/*
|
||
跑点时只需要xy，不需要转角度，
|
||
而且如果跑点时有角度车会呈现蠕动的形态，
|
||
比赛的时候只需要纠正角度，不需要跑点，
|
||
只是为了方便拟合，而且跑点要准的话要加pid，
|
||
目前xy的参数还可以
|
||
*/
|
||
//跑点
|
||
// c->move_vec.Vx = ctrl->nuc.vx*2500;
|
||
// c->move_vec.Vy = ctrl->nuc.vy*2500;
|
||
//纠正角度
|
||
c->move_vec.Vx = ctrl->Vx*95000;
|
||
c->move_vec.Vy = ctrl->Vy*95000;
|
||
c->move_vec.Vw = c->radar_yaw;
|
||
|
||
Buzzer_Control(&c->buzzer_radar_angle,(fabsf(ctrl->nuc.vw) < 1 && ctrl->nuc.vw != 0));
|
||
break;
|
||
|
||
case FORBIDDEN:
|
||
c->move_vec.Vx = ctrl->Vx*ctrl->throttle*9500;
|
||
c->move_vec.Vy = ctrl->Vy*ctrl->throttle*9500;
|
||
c->move_vec.Vw = ctrl->Vw*ctrl->throttle*6000;
|
||
break;
|
||
|
||
case RADAR_RESET:
|
||
c->move_vec.Vx = c->move_sick.Vx;
|
||
c->move_vec.Vy = c->move_sick.Vy;
|
||
c->move_vec.Vw = c->move_sick.Vw;
|
||
|
||
Buzzer_Control(&c->buzzer_sick_calibration,(c->SICK_FALG == 1));
|
||
break;
|
||
}
|
||
|
||
#elif defined(action_sick)
|
||
c->move_vec.Vx =ctrl->C_navi.vx ;
|
||
c->move_vec.Vy =ctrl->C_navi.vy ;
|
||
c->move_vec.Vw =ctrl->C_navi.wz ;
|
||
#endif
|
||
|
||
break;
|
||
}
|
||
|
||
//进行滤波
|
||
c->move_vec.Vx =LowPassFilter2p_Apply(&(c->filled[0]),c->move_vec.Vx);
|
||
c->move_vec.Vy =LowPassFilter2p_Apply(&(c->filled[1]),c->move_vec.Vy);
|
||
c->move_vec.Vw =LowPassFilter2p_Apply(&(c->filled[2]),c->move_vec.Vw);
|
||
|
||
Chassis_speed_calculate(c,pos);
|
||
#ifdef calibration
|
||
#else
|
||
for (uint8_t i = 0 ; i <4 ; i++){
|
||
|
||
c->hopemotorout.motor6020_target[i]=c->hopemotorout.rotor6020_jiesuan_2[i];
|
||
chassis6020_detangle[i] = PID_calc(&(c->pid.chassis_6020anglePid),c->motorfeedback.rotor_angle6020[i],
|
||
c->hopemotorout.motor6020_target[i]);
|
||
c->final_out.final_6020out[i] = PID_calc(&(c->pid.chassis_6020OmegaPid),c->motorfeedback.rotor_rpm6020[i],
|
||
chassis6020_detangle[i]);
|
||
out->chassis6020.as_array[i] = c->final_out.final_6020out[i];
|
||
|
||
c->hopemotorout.motor5065_target[i]=c->hopemotorout.rotor5065_jiesuan_2[i];
|
||
c->final_out.final_5065out[i]=c->hopemotorout.motor5065_target[i];
|
||
out->chassis5065.erpm[i] = c->final_out.final_5065out[i];
|
||
}
|
||
#endif
|
||
//vofa发送
|
||
c->vofa_send[0] =c->sick[0];
|
||
c->vofa_send[1] =c->sick[1];
|
||
c->vofa_send[2] =c->sick[2];
|
||
// c->vofa_send[3] =c->motorfeedback.rotor_rpm5065[0];
|
||
// c->vofa_send[4] =ctrl->nuc.vx;
|
||
// c->vofa_send[5] =ctrl->nuc.vy;
|
||
// c->vofa_send[6] =;
|
||
// c->vofa_send[7] =;
|
||
return CHASSIS_OK;
|
||
}
|