大一寒假——pid在舵机与陀螺仪控制云台稳定——keil5
/** ****************************(C) COPYRIGHT 2019 DJI**************************** * @file pid.c/h * @brief pid实现函数,包括初始化,PID计算函数, * @note * @history * Version Date Author Modification * V1.0.0 Dec-26-2018 RM 1. 完成 * @verbatim ============================================================================== ============================================================================== @endverbatim ****************************(C) COPYRIGHT 2019 DJI**************************** */ #include "pid.h" #include "main.h" #define LimitMax(input, max) \ { \ if (input > max) \ { \ input = max; \ } \ else if (input < -max) \ { \ input = -max; \ } \ } /** * @brief pid struct data init * @param[out] pid: PID struct data point * @param[in] mode: PID_POSITION: normal pid * PID_DELTA: delta pid * @param[in] PID: 0: kp, 1: ki, 2:kd * @param[in] max_out: pid max out * @param[in] max_iout: pid max iout * @retval none */ /** * @brief pid struct data init * @param[out] pid: PID结构数据指针 * @param[in] mode: PID_POSITION:普通PID * PID_DELTA: 差分PID * @param[in] PID: 0: kp, 1: ki, 2:kd * @param[in] max_out: pid最大输出 * @param[in] max_iout: pid最大积分输出 * @retval none */ void PID_init(pid_type_def *pid, uint8_t mode, const fp32 PID[3], fp32 max_out, fp32 max_iout) { if (pid == NULL || PID == NULL) { return; } pid->mode = mode; pid->Kp = PID[0]; pid->Ki = PID[1]; pid->Kd = PID[2]; pid->max_out = max_out; pid->max_iout = max_iout; pid->Dbuf[0] = pid->Dbuf[1] = pid->Dbuf[2] = 0.0f; pid->error[0] = pid->error[1] = pid->error[2] = pid->Pout = pid->Iout = pid->Dout = pid->out = 0.0f; } /** * @brief pid calculate * @param[out] pid: PID struct data point * @param[in] ref: feedback data * @param[in] set: set point * @retval pid out */ /** * @brief pid计算 * @param[out] pid: PID结构数据指针 * @param[in] ref: 反馈数据 * @param[in] set: 设定值 * @retval pid输出 */ fp32 PID_calc(pid_type_def *pid, fp32 ref, fp32 set) { if (pid == NULL) { return 0.0f; } pid->error[2] = pid->error[1]; pid->error[1] = pid->error[0]; pid->set = set; pid->fdb = ref; pid->error[0] = set - ref; if (pid->mode == PID_POSITION) { pid->Pout = pid->Kp * pid->error[0]; pid->Iout += pid->Ki * pid->error[0]; pid->Dbuf[2] = pid->Dbuf[1]; pid->Dbuf[1] = pid->Dbuf[0]; pid->Dbuf[0] = (pid->error[0] - pid->error[1]); pid->Dout = pid->Kd * pid->Dbuf[0]; LimitMax(pid->Iout, pid->max_iout); pid->out = pid->Pout + pid->Iout + pid->Dout; LimitMax(pid->out, pid->max_out); } else if (pid->mode == PID_DELTA) { pid->Pout = pid->Kp * (pid->error[0] - pid->error[1]); pid->Iout = pid->Ki * pid->error[0]; pid->Dbuf[2] = pid->Dbuf[1]; pid->Dbuf[1] = pid->Dbuf[0]; pid->Dbuf[0] = (pid->error[0] - 2.0f * pid->error[1] + pid->error[2]); pid->Dout = pid->Kd * pid->Dbuf[0]; pid->out += pid->Pout + pid->Iout + pid->Dout; LimitMax(pid->out, pid->max_out); } return pid->out; } /** * @brief pid out clear * @param[out] pid: PID struct data point * @retval none */ /** * @brief pid 输出清除 * @param[out] pid: PID结构数据指针 * @retval none */ void PID_clear(pid_type_def *pid) { if (pid == NULL) { return; } pid->error[0] = pid->error[1] = pid->error[2] = 0.0f; pid->Dbuf[0] = pid->Dbuf[1] = pid->Dbuf[2] = 0.0f; pid->out = pid->Pout = pid->Iout = pid->Dout = 0.0f; pid->fdb = pid->set = 0.0f; }
pid.c
#ifndef STRUCT_TYPEDEF_H #define STRUCT_TYPEDEF_H typedef signed char int8_t; typedef signed short int int16_t; typedef signed int int32_t; typedef signed long long int64_t; /* exact-width unsigned integer types */ typedef unsigned char uint8_t; typedef unsigned short int uint16_t; typedef unsigned int uint32_t; typedef unsigned long long uint64_t; typedef unsigned char bool_t; typedef float fp32; typedef double fp64; #endif
struct_typedef.h
/** ****************************(C) COPYRIGHT 2016 DJI**************************** * @file pid.c/h * @brief pid实现函数,包括初始化,PID计算函数, * @note * @history * Version Date Author Modification * V1.0.0 Dec-26-2018 RM 1. 完成 * @verbatim ============================================================================== ============================================================================== @endverbatim ****************************(C) COPYRIGHT 2016 DJI**************************** */ #ifndef PID_H #define PID_H #include "struct_typedef.h" enum PID_MODE { PID_POSITION = 0, PID_DELTA }; typedef struct { uint8_t mode; //PID 三参数 fp32 Kp; fp32 Ki; fp32 Kd; fp32 max_out; //最大输出 fp32 max_iout; //最大积分输出 fp32 set; fp32 fdb; fp32 out; fp32 Pout; fp32 Iout; fp32 Dout; fp32 Dbuf[3]; //微分项 0最新 1上一次 2上上次 fp32 error[3]; //误差项 0最新 1上一次 2上上次 } pid_type_def; /** * @brief pid struct data init * @param[out] pid: PID struct data point * @param[in] mode: PID_POSITION: normal pid * PID_DELTA: delta pid * @param[in] PID: 0: kp, 1: ki, 2:kd * @param[in] max_out: pid max out * @param[in] max_iout: pid max iout * @retval none */ /** * @brief pid struct data init * @param[out] pid: PID结构数据指针 * @param[in] mode: PID_POSITION:普通PID * PID_DELTA: 差分PID * @param[in] PID: 0: kp, 1: ki, 2:kd * @param[in] max_out: pid最大输出 * @param[in] max_iout: pid最大积分输出 * @retval none */ extern void PID_init(pid_type_def *pid, uint8_t mode, const fp32 PID[3], fp32 max_out, fp32 max_iout); /** * @brief pid calculate * @param[out] pid: PID struct data point * @param[in] ref: feedback data * @param[in] set: set point * @retval pid out */ /** * @brief pid计算 * @param[out] pid: PID结构数据指针 * @param[in] ref: 反馈数据 * @param[in] set: 设定值 * @retval pid输出 */ extern fp32 PID_calc(pid_type_def *pid, fp32 ref, fp32 set); /** * @brief pid out clear * @param[out] pid: PID struct data point * @retval none */ /** * @brief pid 输出清除 * @param[out] pid: PID结构数据指针 * @retval none */ extern void PID_clear(pid_type_def *pid); #endif
pid.h
上述为一个反馈的pid代码
此为模拟pid输出网站
PID online simulator - STorM32-BGC Wiki (olliw.eu)
下述为假期期间调试所遇到的问题(针对pid和舵机程序的)
1.舵机旋转需时间,两次过近的命令会导致输出无效。故主程序while(1)中应有delay(ms)以保证有时间转动
2.pid应先从kp开始逐一调参,第一个数值应大于10,以保证有有效输出
3.连线,每次使用应检查是否所有连线都连上了
4.调用函数时,填入数组一定要只保留数组名字,不用&和【】.(因为这个,死活都想不通kp,ki的值为啥传不进函数,而debug而了整整一下午。笨蛋就是我了吧)
5.想要看懂函数内的运算,第一步是把指针学好。(C语言从会到不会系列)
————————————————
使用的模块:
陀螺仪 MPU6050模块 — [野火]STM32模块例程介绍 文档 (embedfire.com)
————————————————
参考资料原文链接: