新增底盘电机功率限制

This commit is contained in:
宋家齐 2024-01-20 16:16:13 +08:00
parent 9e51196992
commit fdcd89b265
11 changed files with 284 additions and 58 deletions

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@ -53,7 +53,7 @@ include_directories(Inc Drivers/STM32F4xx_HAL_Driver/Inc Drivers/STM32F4xx_HAL_D
bsp bsp/adc bsp/can bsp/dwt bsp/flash bsp/gpio bsp/iic bsp/log bsp/pwm bsp/spi bsp/usart bsp/usb bsp bsp/adc bsp/can bsp/dwt bsp/flash bsp/gpio bsp/iic bsp/log bsp/pwm bsp/spi bsp/usart bsp/usb
modules modules/alarm modules/algorithm modules/BMI088 modules/can_comm modules/daemon modules/encoder modules/imu modules/ist8310 modules modules/alarm modules/algorithm modules/BMI088 modules/can_comm modules/daemon modules/encoder modules/imu modules/ist8310
modules/led modules/master_machine modules/message_center modules/motor modules/oled modules/referee modules/remote modules/standard_cmd modules/led modules/master_machine modules/message_center modules/motor modules/oled modules/referee modules/remote modules/standard_cmd
modules/super_cap modules/TFminiPlus modules/unicomm modules/vofa modules/super_cap modules/TFminiPlus modules/unicomm modules/vofa modules/power_meter
modules/motor/DJImotor modules/motor/HTmotor modules/motor/LKmotor modules/motor/servo_motor modules/motor/step_motor modules/motor/ECmotor modules/motor/DJImotor modules/motor/HTmotor modules/motor/LKmotor modules/motor/servo_motor modules/motor/step_motor modules/motor/ECmotor
application application/chassis application/cmd application/gimbal application/shoot application application/chassis application/cmd application/gimbal application/shoot
Middlewares/Third_Party/SEGGER/RTT Middlewares/Third_Party/SEGGER/Config) Middlewares/Third_Party/SEGGER/RTT Middlewares/Third_Party/SEGGER/Config)

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@ -17,6 +17,7 @@
#include "super_cap.h" #include "super_cap.h"
#include "message_center.h" #include "message_center.h"
#include "referee_task.h" #include "referee_task.h"
#include "power_meter.h"
#include "general_def.h" #include "general_def.h"
#include "bsp_dwt.h" #include "bsp_dwt.h"
@ -46,6 +47,7 @@ static referee_info_t* referee_data; // 用于获取裁判系统的数据
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 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
static SuperCapInstance *cap; // 超级电容 static SuperCapInstance *cap; // 超级电容
static PowerMeterInstance *power_meter; //功率计
static DJIMotorInstance *motor_lf, *motor_rf, *motor_lb, *motor_rb; // left right forward back static DJIMotorInstance *motor_lf, *motor_rf, *motor_lb, *motor_rb; // left right forward back
/* 用于自旋变速策略的时间变量 */ /* 用于自旋变速策略的时间变量 */
@ -55,6 +57,8 @@ static DJIMotorInstance *motor_lf, *motor_rf, *motor_lb, *motor_rb; // left righ
static float chassis_vx, chassis_vy; // 将云台系的速度投影到底盘 static float chassis_vx, chassis_vy; // 将云台系的速度投影到底盘
static float vt_lf, vt_rf, vt_lb, vt_rb; // 底盘速度解算后的临时输出,待进行限幅 static float vt_lf, vt_rf, vt_lb, vt_rb; // 底盘速度解算后的临时输出,待进行限幅
static const float motor_power_K[3] = {1.6301e-6f,5.7501e-7f,2.5863e-7f};
void ChassisInit() void ChassisInit()
{ {
// 四个轮子的参数一样,改tx_id和反转标志位即可 // 四个轮子的参数一样,改tx_id和反转标志位即可
@ -82,7 +86,9 @@ void ChassisInit()
.angle_feedback_source = MOTOR_FEED, .angle_feedback_source = MOTOR_FEED,
.speed_feedback_source = MOTOR_FEED, .speed_feedback_source = MOTOR_FEED,
.outer_loop_type = SPEED_LOOP, .outer_loop_type = SPEED_LOOP,
.close_loop_type = SPEED_LOOP,//| CURRENT_LOOP, .close_loop_type = SPEED_LOOP| CURRENT_LOOP,
.power_limit_flag = POWER_LIMIT_ON, //开启功率限制
}, },
.motor_type = M3508, .motor_type = M3508,
}; };
@ -114,6 +120,15 @@ void ChassisInit()
}}; }};
cap = SuperCapInit(&cap_conf); // 超级电容初始化 cap = SuperCapInit(&cap_conf); // 超级电容初始化
PowerMeter_Init_Config_s power_conf = {
.can_config = {
.can_handle = &hcan1,
.rx_id = 0x212,
}
};
power_meter = PowerMeterInit(&power_conf);
// 发布订阅初始化,如果为双板,则需要can comm来传递消息 // 发布订阅初始化,如果为双板,则需要can comm来传递消息
#ifdef CHASSIS_BOARD #ifdef CHASSIS_BOARD
Chassis_IMU_data = INS_Init(); // 底盘IMU初始化 Chassis_IMU_data = INS_Init(); // 底盘IMU初始化
@ -165,21 +180,47 @@ static void OmniCalculate()
vt_lf/=(WHEEL_BASE*1.414f); vt_lf/=(WHEEL_BASE*1.414f);
} }
//依据3508电机功率模型预测电机输出功率
static float EstimatePower(DJIMotorInstance* chassis_motor)
{
float I_cmd = chassis_motor->motor_controller.current_PID.Output;
float w = chassis_motor->measure.speed_aps /6 ;//aps to rpm
float power = motor_power_K[0] * I_cmd * w + motor_power_K[1]*w*w + motor_power_K[2]*I_cmd*I_cmd;
return power;
}
float vofa_send_data[6];
/** /**
* @brief * @brief
* *
*/ */
static void LimitChassisOutput() static void LimitChassisOutput()
{ {
// 功率限制待添加 float P_cmd = motor_rf->motor_controller.motor_power_predict +
// referee_data->PowerHeatData.chassis_power; motor_rb->motor_controller.motor_power_predict +
// referee_data->PowerHeatData.chassis_power_buffer; motor_lb->motor_controller.motor_power_predict +
motor_lf->motor_controller.motor_power_predict + 3.6f;
float P_max = 60 - 10;
float K = P_max/P_cmd;
vofa_send_data[2] = P_cmd;
motor_rf->motor_controller.motor_power_scale = K;
motor_rb->motor_controller.motor_power_scale = K;
motor_lf->motor_controller.motor_power_scale = K;
motor_lb->motor_controller.motor_power_scale = K;
{
DJIMotorSetRef(motor_lf, vt_lf);
DJIMotorSetRef(motor_rf, vt_rf);
DJIMotorSetRef(motor_lb, vt_lb);
DJIMotorSetRef(motor_rb, vt_rb);
}
// 完成功率限制后进行电机参考输入设定
DJIMotorSetRef(motor_lf, vt_lf);
DJIMotorSetRef(motor_rf, vt_rf);
DJIMotorSetRef(motor_lb, vt_lb);
DJIMotorSetRef(motor_rb, vt_rb);
} }
/** /**
@ -246,16 +287,28 @@ void ChassisTask()
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;
motor_rf->motor_controller.motor_power_max = 10;
// 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
//MecanumCalculate(); //MecanumCalculate();
OmniCalculate(); OmniCalculate();
//vt_rf = 5000;
// 根据裁判系统的反馈数据和电容数据对输出限幅并设定闭环参考值 // 根据裁判系统的反馈数据和电容数据对输出限幅并设定闭环参考值
LimitChassisOutput(); LimitChassisOutput();
// float vofa_send_data[2];
// vofa_send_data[0]=motor_lb->motor_controller.speed_PID.Ref; //DJIMotorSetRef(motor_rf, 5000);
// vofa_send_data[1]=motor_lb->motor_controller.speed_PID.Measure;
// vofa_justfloat_output(vofa_send_data,8,&huart1);
vofa_send_data[0] = motor_rf->motor_controller.speed_PID.Ref;
vofa_send_data[1] = motor_rf->motor_controller.speed_PID.Measure;
vofa_send_data[3] = PowerMeterGet(power_meter);
vofa_send_data[4] = 60;
vofa_justfloat_output(vofa_send_data,24,&huart1);
// 根据电机的反馈速度和IMU(如果有)计算真实速度 // 根据电机的反馈速度和IMU(如果有)计算真实速度
EstimateSpeed(); EstimateSpeed();

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@ -157,6 +157,9 @@ static void RemoteControlSet()
shoot_cmd_send.load_mode = LOAD_STOP; shoot_cmd_send.load_mode = LOAD_STOP;
// 射频控制,固定每秒1发,后续可以根据左侧拨轮的值大小切换射频, // 射频控制,固定每秒1发,后续可以根据左侧拨轮的值大小切换射频,
shoot_cmd_send.shoot_rate = 8; shoot_cmd_send.shoot_rate = 8;
//检测到卡弹 拨弹盘反转
if(shoot_fetch_data.stalled_flag == 1)
shoot_cmd_send.load_mode = LOAD_REVERSE;
} }
/** /**

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@ -9,10 +9,13 @@
#include "bmi088.h" #include "bmi088.h"
#include "vofa.h" #include "vofa.h"
#include "power_meter.h"
static attitude_t *gimba_IMU_data; // 云台IMU数据 static attitude_t *gimba_IMU_data; // 云台IMU数据
static DJIMotorInstance *yaw_motor, *pitch_motor; static DJIMotorInstance *yaw_motor, *pitch_motor;
static ECMotorInstance *big_yaw_motor; static DJIMotorInstance *big_yaw_motor;
static Publisher_t *gimbal_pub; // 云台应用消息发布者(云台反馈给cmd) static Publisher_t *gimbal_pub; // 云台应用消息发布者(云台反馈给cmd)
static Subscriber_t *gimbal_sub; // cmd控制消息订阅者 static Subscriber_t *gimbal_sub; // cmd控制消息订阅者
@ -110,14 +113,16 @@ void GimbalInit()
.close_loop_type = OPEN_LOOP, .close_loop_type = OPEN_LOOP,
.motor_reverse_flag = MOTOR_DIRECTION_NORMAL, .motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
}, },
.motor_type = ECA8210 .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);
// pitch_motor = DJIMotorInit(&pitch_config); // pitch_motor = DJIMotorInit(&pitch_config);
big_yaw_motor = ECMotorInit(&big_yaw_config); //big_yaw_motor = ECMotorInit(&big_yaw_config);
//big_yaw_motor = DJIMotorInit(&big_yaw_config);
gimbal_pub = PubRegister("gimbal_feed", sizeof(Gimbal_Upload_Data_s)); gimbal_pub = PubRegister("gimbal_feed", sizeof(Gimbal_Upload_Data_s));
gimbal_sub = SubRegister("gimbal_cmd", sizeof(Gimbal_Ctrl_Cmd_s)); gimbal_sub = SubRegister("gimbal_cmd", sizeof(Gimbal_Ctrl_Cmd_s));
@ -172,41 +177,43 @@ void GimbalTask()
// ... // ...
//DJIMotorEnable(pitch_motor); //DJIMotorEnable(pitch_motor);
ECMotorEnable(big_yaw_motor); //ECMotorEnable(big_yaw_motor);
float input = step_input_generate(&sinInputGenerate);
float input = sin_input_generate(&sinInputGenerate);
//DJIMotorEnable(big_yaw_motor);
//DJIMotorSetRef(pitch_motor,input); //DJIMotorSetRef(pitch_motor,input);
ECMotorSetRef(big_yaw_motor,30); //ECMotorSetRef(big_yaw_motor,30);
//ANODT_SendF1(input*1000,pitch_motor->measure.speed_aps*1000,0,0); //ANODT_SendF1(input*1000,pitch_motor->measure.speed_aps*1000,0,0);
float theta = pitch_motor->measure.angle_single_round - 6200 * ECD_ANGLE_COEF_DJI; float theta = pitch_motor->measure.angle_single_round - 6200 * ECD_ANGLE_COEF_DJI;
float gravity_feed = 3800*arm_cos_f32(theta/180*PI); float gravity_feed = 3800*arm_cos_f32(theta/180*PI);
//DJIMotorSetRef(pitch_motor,gravity_feed); //DJIMotorSetRef(big_yaw_motor,input+2000);
float vofa_send_data[4]; // float vofa_send_data[6];
vofa_send_data[0]=big_yaw_motor->measure.speed_rads; // vofa_send_data[0]=big_yaw_motor->measure.speed_aps;
vofa_send_data[1]=big_yaw_motor->measure.angle_single_round; // vofa_send_data[1]=big_yaw_motor->measure.angle_single_round;
vofa_send_data[2]=big_yaw_motor->measure.real_current; // vofa_send_data[2]=big_yaw_motor->measure.real_current;
vofa_send_data[3]=big_yaw_motor->measure.temperature; // vofa_send_data[3]=power_meter->power_msg.vol;
// vofa_send_data[3]=yaw_motor->motor_controller.angle_PID.Measure; // vofa_send_data[4]=power_meter->power_msg.current;
vofa_justfloat_output(vofa_send_data,16,&huart1); // vofa_send_data[5]=big_yaw_motor->motor_controller.pid_ref;
//
// vofa_justfloat_output(vofa_send_data,24,&huart1);
vofa_send_data[0] = pitch_motor->motor_controller.pid_ref; // vofa_send_data[0] = pitch_motor->motor_controller.pid_ref;
vofa_send_data[1] = pitch_motor->measure.real_current; // vofa_send_data[1] = pitch_motor->measure.real_current;
vofa_send_data[2] = theta; // vofa_send_data[2] = theta;
vofa_send_data[3] = gravity_feed; // vofa_send_data[3] = gravity_feed;
vofa_justfloat_output(vofa_send_data,16,&huart1); // vofa_justfloat_output(vofa_send_data,16,&huart1);
// 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;
//
// 推送消息 // // 推送消息
PubPushMessage(gimbal_pub, (void *)&gimbal_feedback_data); // PubPushMessage(gimbal_pub, (void *)&gimbal_feedback_data);
} }
@ -260,6 +267,7 @@ float sin_input_generate(sin_input_generate_t* InputGenerate)
else else
InputGenerate->input = arm_sin_f32(2*PI*InputGenerate->frequency[InputGenerate->frequency_index]*InputGenerate->time); InputGenerate->input = arm_sin_f32(2*PI*InputGenerate->frequency[InputGenerate->frequency_index]*InputGenerate->time);
//float input = arm_sin_f32(2*PI*frequency*time); //float input = arm_sin_f32(2*PI*frequency*time);
InputGenerate->input *= 2000;
return InputGenerate->input; return InputGenerate->input;
} }

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@ -31,13 +31,13 @@ void RobotInit()
#if defined(ONE_BOARD) || defined(GIMBAL_BOARD) #if defined(ONE_BOARD) || defined(GIMBAL_BOARD)
RobotCMDInit(); RobotCMDInit();
//暂时注释云台和发射任务 调试底盘
GimbalInit(); GimbalInit();
// ShootInit(); ShootInit();
#endif #endif
#if defined(ONE_BOARD) || defined(CHASSIS_BOARD) #if defined(ONE_BOARD) || defined(CHASSIS_BOARD)
//ChassisInit(); ChassisInit();
#endif #endif
OSTaskInit(); // 创建基础任务 OSTaskInit(); // 创建基础任务
@ -52,11 +52,11 @@ void RobotTask()
RobotCMDTask(); RobotCMDTask();
//暂时注释云台和发射任务 调试底盘 //暂时注释云台和发射任务 调试底盘
GimbalTask(); GimbalTask();
// ShootTask(); ShootTask();
#endif #endif
#if defined(ONE_BOARD) || defined(CHASSIS_BOARD) #if defined(ONE_BOARD) || defined(CHASSIS_BOARD)
//ChassisTask(); ChassisTask();
#endif #endif
} }

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@ -19,7 +19,7 @@
/* 开发板类型定义,烧录时注意不要弄错对应功能;修改定义后需要重新编译,只能存在一个定义! */ /* 开发板类型定义,烧录时注意不要弄错对应功能;修改定义后需要重新编译,只能存在一个定义! */
#define ONE_BOARD // 单板控制整车 #define ONE_BOARD // 单板控制整车
// #define CHASSIS_BOARD //底盘板 // #define CHASSIS_BOARD //底盘板
// #define GIMBAL_BOARD //云台板 //#define GIMBAL_BOARD //云台板
#define VISION_USE_VCP // 使用虚拟串口发送视觉数据 #define VISION_USE_VCP // 使用虚拟串口发送视觉数据
// #define VISION_USE_UART // 使用串口发送视觉数据 // #define VISION_USE_UART // 使用串口发送视觉数据
@ -204,6 +204,7 @@ typedef struct
{ {
// code to go here // code to go here
// ... // ...
uint8_t stalled_flag; //堵转标志
} Shoot_Upload_Data_s; } Shoot_Upload_Data_s;
#pragma pack() // 开启字节对齐,结束前面的#pragma pack(1) #pragma pack() // 开启字节对齐,结束前面的#pragma pack(1)

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@ -16,7 +16,7 @@ static Subscriber_t *shoot_sub;
static Shoot_Upload_Data_s shoot_feedback_data; // 来自cmd的发射控制信息 static Shoot_Upload_Data_s shoot_feedback_data; // 来自cmd的发射控制信息
// dwt定时,计算冷却用 // dwt定时,计算冷却用
static float hibernate_time = 0, dead_time = 0; static float hibernate_time = 0,last_hibernate_time = 0, dead_time = 0;
void ShootInit() void ShootInit()
{ {
@ -48,7 +48,7 @@ void ShootInit()
.speed_feedback_source = MOTOR_FEED, .speed_feedback_source = MOTOR_FEED,
.outer_loop_type = SPEED_LOOP, .outer_loop_type = SPEED_LOOP,
.close_loop_type = SPEED_LOOP | CURRENT_LOOP, .close_loop_type = SPEED_LOOP,
.motor_reverse_flag = MOTOR_DIRECTION_NORMAL, .motor_reverse_flag = MOTOR_DIRECTION_NORMAL,
}, },
.motor_type = M3508}; .motor_type = M3508};
@ -74,12 +74,12 @@ void ShootInit()
.MaxOut = 200, .MaxOut = 200,
}, },
.speed_PID = { .speed_PID = {
.Kp = 0, // 10 .Kp = 3, // 10
.Ki = 0, // 1 .Ki = 0, // 1
.Kd = 0, .Kd = 0,
.Improve = PID_Integral_Limit, .Improve = PID_Integral_Limit,
.IntegralLimit = 5000, .IntegralLimit = 5000,
.MaxOut = 5000, .MaxOut = 10000,
}, },
.current_PID = { .current_PID = {
.Kp = 0, // 0.7 .Kp = 0, // 0.7
@ -103,6 +103,31 @@ void ShootInit()
shoot_pub = PubRegister("shoot_feed", sizeof(Shoot_Upload_Data_s)); shoot_pub = PubRegister("shoot_feed", sizeof(Shoot_Upload_Data_s));
shoot_sub = SubRegister("shoot_cmd", sizeof(Shoot_Ctrl_Cmd_s)); shoot_sub = SubRegister("shoot_cmd", sizeof(Shoot_Ctrl_Cmd_s));
} }
//卡弹检测
void stalled_detect()
{
static float last_detect_time = 0,detect_time = 0;
static float last_total_angle = 0;
static uint8_t stalled_cnt = 0;
last_detect_time = detect_time;
detect_time = DWT_GetTimeline_ms();
if(detect_time - last_detect_time < 200) // 200ms 检测一次
return;
if(shoot_cmd_recv.load_mode == LOAD_BURSTFIRE)
{
float reference_angle = (detect_time - last_detect_time) * loader->motor_controller.pid_ref * 1e3f;
float real_angle = loader->measure.total_angle - last_total_angle;
if(real_angle < reference_angle * 0.2f)
{
//stalled_cnt ++;
shoot_feedback_data.stalled_flag = 1;
}
}
}
/* 机器人发射机构控制核心任务 */ /* 机器人发射机构控制核心任务 */
void ShootTask() void ShootTask()
@ -126,8 +151,8 @@ void ShootTask()
// 如果上一次触发单发或3发指令的时间加上不应期仍然大于当前时间(尚未休眠完毕),直接返回即可 // 如果上一次触发单发或3发指令的时间加上不应期仍然大于当前时间(尚未休眠完毕),直接返回即可
// 单发模式主要提供给能量机关激活使用(以及英雄的射击大部分处于单发) // 单发模式主要提供给能量机关激活使用(以及英雄的射击大部分处于单发)
// if (hibernate_time + dead_time > DWT_GetTimeline_ms()) if (hibernate_time + dead_time > DWT_GetTimeline_ms())
// return; return;
// 若不在休眠状态,根据robotCMD传来的控制模式进行拨盘电机参考值设定和模式切换 // 若不在休眠状态,根据robotCMD传来的控制模式进行拨盘电机参考值设定和模式切换
switch (shoot_cmd_recv.load_mode) switch (shoot_cmd_recv.load_mode)
@ -155,12 +180,17 @@ void ShootTask()
case LOAD_BURSTFIRE: case LOAD_BURSTFIRE:
DJIMotorOuterLoop(loader, SPEED_LOOP); DJIMotorOuterLoop(loader, SPEED_LOOP);
DJIMotorSetRef(loader, shoot_cmd_recv.shoot_rate * 360 * REDUCTION_RATIO_LOADER / 8); DJIMotorSetRef(loader, shoot_cmd_recv.shoot_rate * 360 * REDUCTION_RATIO_LOADER / 8);
// x颗/秒换算成速度: 已知一圈的载弹量,由此计算出1s需要转的角度,注意换算角速度(DJIMotor的速度单位是angle per second)
// x颗/秒换算成速度: 已知一圈的载弹量,由此计算出1s需要转的角度,注意换算角速度(DJIMotor的速度单位是angle per second)
break; break;
// 拨盘反转,对速度闭环,后续增加卡弹检测(通过裁判系统剩余热量反馈和电机电流) // 拨盘反转,对速度闭环,后续增加卡弹检测(通过裁判系统剩余热量反馈和电机电流)
// 也有可能需要从switch-case中独立出来 // 也有可能需要从switch-case中独立出来
case LOAD_REVERSE: case LOAD_REVERSE:
DJIMotorOuterLoop(loader, SPEED_LOOP); DJIMotorOuterLoop(loader, SPEED_LOOP);
DJIMotorSetRef(loader, 8 * 360 * REDUCTION_RATIO_LOADER / 8); // 固定速度反转
hibernate_time = DWT_GetTimeline_ms(); // 记录触发指令的时间
dead_time = 500; // 翻转500ms
shoot_feedback_data.stalled_flag = 0 ; //清除堵转标志
// ... // ...
break; break;
default: default:
@ -207,6 +237,8 @@ void ShootTask()
{ {
//... //...
} }
//卡弹检测
stalled_detect();
// 反馈数据,目前暂时没有要设定的反馈数据,后续可能增加应用离线监测以及卡弹反馈 // 反馈数据,目前暂时没有要设定的反馈数据,后续可能增加应用离线监测以及卡弹反馈
PubPushMessage(shoot_pub, (void *)&shoot_feedback_data); PubPushMessage(shoot_pub, (void *)&shoot_feedback_data);

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@ -198,6 +198,7 @@ DJIMotorInstance *DJIMotorInit(Motor_Init_Config_s *config)
instance->motor_controller.speed_feedforward_ptr = config->controller_param_init_config.speed_feedforward_ptr; instance->motor_controller.speed_feedforward_ptr = config->controller_param_init_config.speed_feedforward_ptr;
// 后续增加电机前馈控制器(速度和电流) // 后续增加电机前馈控制器(速度和电流)
// 电机分组,因为至多4个电机可以共用一帧CAN控制报文 // 电机分组,因为至多4个电机可以共用一帧CAN控制报文
MotorSenderGrouping(instance, &config->can_init_config); MotorSenderGrouping(instance, &config->can_init_config);
@ -251,6 +252,16 @@ void DJIMotorSetRef(DJIMotorInstance *motor, float ref)
{ {
motor->motor_controller.pid_ref = ref; motor->motor_controller.pid_ref = ref;
} }
static const float motor_power_K[3] = {1.6301e-6f,5.7501e-7f,2.5863e-7f};
//依据3508电机功率模型预测电机输出功率
static float EstimatePower(DJIMotorInstance* chassis_motor,float output)
{
float I_cmd = chassis_motor->motor_controller.current_PID.Output;
float w = chassis_motor->measure.speed_aps /6 ;//aps to rpm
float power = motor_power_K[0] * I_cmd * w + motor_power_K[1]*w*w + motor_power_K[2]*I_cmd*I_cmd;
return power;
}
// 为所有电机实例计算三环PID,发送控制报文 // 为所有电机实例计算三环PID,发送控制报文
void DJIMotorControl() void DJIMotorControl()
@ -274,7 +285,6 @@ void DJIMotorControl()
pid_ref = motor_controller->pid_ref; // 保存设定值,防止motor_controller->pid_ref在计算过程中被修改 pid_ref = motor_controller->pid_ref; // 保存设定值,防止motor_controller->pid_ref在计算过程中被修改
if (motor_setting->motor_reverse_flag == MOTOR_DIRECTION_REVERSE) if (motor_setting->motor_reverse_flag == MOTOR_DIRECTION_REVERSE)
pid_ref *= -1; // 设置反转 pid_ref *= -1; // 设置反转
// pid_ref会顺次通过被启用的闭环充当数据的载体 // pid_ref会顺次通过被启用的闭环充当数据的载体
// 计算位置环,只有启用位置环且外层闭环为位置时会计算速度环输出 // 计算位置环,只有启用位置环且外层闭环为位置时会计算速度环输出
if ((motor_setting->close_loop_type & ANGLE_LOOP) && motor_setting->outer_loop_type == ANGLE_LOOP) if ((motor_setting->close_loop_type & ANGLE_LOOP) && motor_setting->outer_loop_type == ANGLE_LOOP)
@ -308,6 +318,7 @@ void DJIMotorControl()
{ {
//现在3508和6020电调都内置电流闭环 无需PID计算 //现在3508和6020电调都内置电流闭环 无需PID计算
//pid_ref = PIDCalculate(&motor_controller->current_PID, measure->real_current, pid_ref); //pid_ref = PIDCalculate(&motor_controller->current_PID, measure->real_current, pid_ref);
motor_controller->current_PID.Output = pid_ref;
pid_ref = pid_ref; pid_ref = pid_ref;
} }
@ -316,6 +327,35 @@ void DJIMotorControl()
if (motor_setting->feedback_reverse_flag == FEEDBACK_DIRECTION_REVERSE) if (motor_setting->feedback_reverse_flag == FEEDBACK_DIRECTION_REVERSE)
pid_ref *= -1; pid_ref *= -1;
//功率限制
if(motor_setting->power_limit_flag == POWER_LIMIT_ON)
{
float I_cmd = pid_ref;
float w = measure->speed_aps /6 ;//aps to rpm
motor_controller->motor_power_predict = motor_power_K[0] * I_cmd * w + motor_power_K[1]*w*w + motor_power_K[2]*I_cmd*I_cmd;
//这里K应该使用所有底盘电机一起计算 (在底盘任务中)
//float K = motor_controller->motor_power_max / motor_controller->motor_power_predict;
float K = motor_controller->motor_power_scale;
if(K>=1 || motor_controller->motor_power_predict < 0)//未超过最大功率 或做负功的电机 不做限制
{
}
else if(K<1)
{
float P_cmd = K * motor_controller->motor_power_predict; //对输出功率进行缩放
float a = motor_power_K[2] ;
float b = motor_power_K[0] * w;
float c = motor_power_K[1] * w * w - P_cmd;
if(pid_ref < 0)
pid_ref = (-b - sqrtf(b*b-4*a*c))/(2*a);
else
pid_ref = (-b + sqrtf(b*b-4*a*c))/(2*a);
}
//if( motor_controller->motor_power_predict < )
}
// 获取最终输出 // 获取最终输出
set = (int16_t)pid_ref; set = (int16_t)pid_ref;

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@ -68,6 +68,11 @@ typedef enum
MOTOR_ENALBED = 1, MOTOR_ENALBED = 1,
} Motor_Working_Type_e; } Motor_Working_Type_e;
typedef enum
{
NO_POWER_LIMIT = 0,
POWER_LIMIT_ON = 1,
} Power_Limit_Type_e;
/* 电机控制设置,包括闭环类型,反转标志和反馈来源 */ /* 电机控制设置,包括闭环类型,反转标志和反馈来源 */
typedef struct typedef struct
{ {
@ -79,6 +84,8 @@ typedef struct
Feedback_Source_e speed_feedback_source; // 速度反馈类型 Feedback_Source_e speed_feedback_source; // 速度反馈类型
Feedfoward_Type_e feedforward_flag; // 前馈标志 Feedfoward_Type_e feedforward_flag; // 前馈标志
Power_Limit_Type_e power_limit_flag; //功率限制标志
} Motor_Control_Setting_s; } Motor_Control_Setting_s;
/* 电机控制器,包括其他来源的反馈数据指针,3环控制器和电机的参考输入*/ /* 电机控制器,包括其他来源的反馈数据指针,3环控制器和电机的参考输入*/
@ -95,6 +102,10 @@ typedef struct
PIDInstance angle_PID; PIDInstance angle_PID;
float pid_ref; // 将会作为每个环的输入和输出顺次通过串级闭环 float pid_ref; // 将会作为每个环的输入和输出顺次通过串级闭环
float motor_power_max; //每个电机分配的功率上限
float motor_power_predict; //根据模型预测的电机功率
float motor_power_scale; //电机功率缩放比例
} Motor_Controller_s; } Motor_Controller_s;
/* 电机类型枚举 */ /* 电机类型枚举 */
@ -143,6 +154,7 @@ typedef struct
Motor_Type_e motor_type; Motor_Type_e motor_type;
CAN_Init_Config_s can_init_config; CAN_Init_Config_s can_init_config;
Motor_Control_Type_e motor_control_type; Motor_Control_Type_e motor_control_type;
} Motor_Init_Config_s; } Motor_Init_Config_s;
#endif // !MOTOR_DEF_H #endif // !MOTOR_DEF_H

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@ -0,0 +1,38 @@
//
// Created by SJQ on 2023/12/19.
//
#include "power_meter.h"
#include "memory.h"
#include "stdlib.h"
static PowerMeterInstance *power_meter_instance = NULL; // 可以由app保存此指针
static void PowerMeterRxCallback(CANInstance *_instance)
{
uint8_t *rxbuff;
PowerMeter_Msg_s *Msg;
rxbuff = _instance->rx_buff;
Msg = &power_meter_instance->power_msg;
Msg->vol = (uint16_t)(rxbuff[1] << 8 | rxbuff[0]);
Msg->current = (uint16_t)(rxbuff[3] << 8 | rxbuff[2]);
}
PowerMeterInstance *PowerMeterInit(PowerMeter_Init_Config_s *PowerMeter_config)
{
power_meter_instance = (PowerMeterInstance *)malloc(sizeof(PowerMeterInstance));
memset(power_meter_instance, 0, sizeof(PowerMeterInstance));
PowerMeter_config->can_config.can_module_callback = PowerMeterRxCallback;
power_meter_instance->can_ins = CANRegister(&PowerMeter_config->can_config);
return power_meter_instance;
}
float PowerMeterGet(PowerMeterInstance *instance)
{
float power = instance->power_msg.current*instance->power_msg.vol/1e4;
return power;
}
#include "power_meter.h"

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@ -0,0 +1,39 @@
//
// Created by SJQ on 2023/12/19.
//
#ifndef BASIC_FRAMEWORK_POWER_METER_H
#define BASIC_FRAMEWORK_POWER_METER_H
#include "bsp_can.h"
#pragma pack(1)
typedef struct
{
uint16_t vol; // 电压
uint16_t current; // 电流
} PowerMeter_Msg_s;
#pragma pack()
/* 超级电容实例 */
typedef struct
{
CANInstance *can_ins; // CAN实例
PowerMeter_Msg_s power_msg; // 功率计反馈信息
} PowerMeterInstance;
/* 超级电容初始化配置 */
typedef struct
{
CAN_Init_Config_s can_config;
} PowerMeter_Init_Config_s;
/**
* @brief
*
* @param PowerMeter_config
* @return PowerMeterInstance*
*/
PowerMeterInstance *PowerMeterInit(PowerMeter_Init_Config_s *PowerMeter_config);
float PowerMeterGet(PowerMeterInstance *instance);
#endif //BASIC_FRAMEWORK_POWER_METER_H