344 lines
10 KiB
C
344 lines
10 KiB
C
/*
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滑膜面调参目标使滑模面s趋近于0，趋近率选择：
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指数趋近率
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幂次趋近率
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J给个固定的值，乘一个输出，J的大小取决于控制量受噪声影响
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IMU噪声对其影响很大，J应该给大些，并且K和s不能给太大，如果基于编码器控制J建议直接给1
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ε(epsilon)不宜过大，过大会影响精度,limit和ε给的值决定线性区间
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K是增益，K大了也会抖,并且影响到目标位置是否能停下来，K太大会停不下来
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c决定s趋近0的快满程度，c大了会抖
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注意，滑膜控制是位置控制，这个位置变化是在控制频率内的，我的速度也要乘这个时间如（0.002）
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否则速度误差占比会非常大，电机停不下来
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输出u
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参考资料
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https://zhuanlan.zhihu.com/p/78549442
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*/
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#include "Sliding.h"
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#include "math.h"
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#include "user_math.h"
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/**
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* @brief 参数调整时使其连续
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*
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* @param Sliding s结构体
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*/
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static void OutContinuation(Sliding *s){
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if(s->param->K != 0 && s->param->c2 != 0)
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{
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s->position.error_integral = (s->param_last->K / s->param->K) * (s->param_last->c2 / s->param->c2) * s->position.error_integral;
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s->velocity.error_integral = (s->param_last->K / s->param->K) * (s->param_last->c2 / s->param->c2) * s->velocity.error_integral;
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}
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s->param_last = s->param;
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}
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/**
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* @brief 符号函数
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*
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* @param s 滑膜面
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* @return
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*/
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static float Signal(float s){
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if (s > 0)
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return 1;
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else if (s == 0)
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return 0;
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else
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return -1;
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}
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/**
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* @brief 饱和函数
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*滑模控制中用于代替符号函数的连续化近似函数，用于抑制滑模控制的高频抖振现象。
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函数特性：
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在滑模面 s 较小时（边界层内），输出与输入呈线性关系
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在滑模面 s 较大时（边界层外），输出饱和为 ±1
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连续可导（在边界点一阶连续），减少控制系统的高频切换
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* @param s 滑膜面
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* @param sliding 滑膜结构体
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* @return Signal(y)/y
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*/
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static float Sat(float s,Sliding *sliding){
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float y;
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y = s / sliding->param->epsilon;
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if (fabs(y) <= sliding->param->limit)
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return y;
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else
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return Signal(y);
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}
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/**
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* @brief 滑膜设立参数
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*
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* @param Sliding s结构体
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* @param mode 滑膜模式
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* @param param 滑膜参数
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* @return
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*/
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static void SMC_SetParam(Sliding *s,Smc_mode mode,SlidingParam *param) {
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///EXPONENT,POWER,VELSMC 参数设定
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s->mode = mode;
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switch(mode){
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case EXPONENT:
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case POWER:
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case VELSMC:
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s->param = param;
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OutContinuation(s);
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break;
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case TFSMC:
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break;
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case EISMC:
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s->param = param;
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OutContinuation(s);
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break;
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}
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}
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/**
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* @brief 滑膜重置
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*
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* @param Sliding s结构体
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* @return
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*/
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void SMC_Reset(Sliding *s){
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/* 位置速度清零 */
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s->position.tar_now = 0;
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s->position.tar_last = 0;
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s->position.tar_differential = 0;
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s->velocity.tar_now = 0;
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s->velocity.tar_last = 0;
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s->velocity.tar_differential = 0;
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/* 误差清零 */
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s->position.error = 0;
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s->velocity.error = 0;
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s->position.error_eps = 0;
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s->velocity.error_eps = 0;
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s->position.now_get = 0;
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s->velocity.now_get = 0;
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/* 一阶导清零 */
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s->velocity.tar_differential_last=0;
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s->position.tar_differential_second=0;
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s->position.tar_differential_last=0;
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/* 积分清零 */
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s->position.error_integral=0;
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s->velocity.error_integral = 0;
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}
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/**
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* @brief 滑膜初始化，设立参数
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*
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* @param Sliding s结构体
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* @param mode 滑膜模式
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* @param param 滑膜参数
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* @return
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*/
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void SMC_Init(Sliding *s,Smc_mode mode,SlidingParam *param){
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s->J = 0;
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s->param->K = 0;
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s->param->c = 0;
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s->param->epsilon = 0;
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s->param->u_max = 0;
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s->param->limit = 0;
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s->position.tar_now = 0;
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s->position.tar_last = 0;
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s->position.tar_differential = 0;
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s->position.error = 0;
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s->velocity.error = 0;
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s->velocity.error_integral = 0;
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s->velocity.error_integral_max = 0;
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s->position.error_eps = 0;
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s->velocity.error_eps = 0;
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s->position.now_get = 0;
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s->velocity.now_get = 0;
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/* 设立参数 */
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SMC_SetParam(s,mode,param);
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}
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/**
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* @brief 位置环速度更新
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*
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* @param Sliding s结构体
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* @param target 目标位置
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* @param pos_now 现在位置
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* @param vol_now 现在速度
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* @param dt 采样频率
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* @return
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*/
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void SMC_PErrorUpdate(Sliding *s,float target, float pos_now, float vol_now,float dt) {
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s->position.tar_now = target;
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/* 一阶导(速度) */
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s->position.tar_differential = (float)((s->position.tar_now - s->position.tar_last)/dt);
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/* 二阶导 */
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s->position.tar_differential_second=(float)((s->position.tar_differential- s->position.tar_differential_last)/dt);
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s->position.error = pos_now - target;
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s->velocity.error = vol_now - s->position.tar_differential;
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/* 更新上一次的值 */
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s->position.tar_last = s->position.tar_now;
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/* 位置误差积分项 */
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s->position.error_integral += (float)(s->position.error * dt);
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/* 二阶导更新 */
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s->position.tar_differential_last = s->position.tar_differential;
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}
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/**
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* @brief 速度环误差更新
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*
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* @param Sliding s结构体
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* @param target 目标位置
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* @param vol_now 现在速度
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* @param dt 采样频率
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* @return
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*/
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void SMC_VErrorUpdate(Sliding *s,float target,float vol_now,float dt) {
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s->velocity.tar_now = target;
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s->velocity.tar_differential = (float)((s->velocity.tar_now - s->velocity.tar_last)/dt);
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// smc.error.tar_differential_second = (float)((smc.error.tar_differential- smc.error.tar_differential_last)/SAMPLE_PERIOD); ///二阶导
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s->velocity.error = vol_now - s->velocity.tar_now;
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/* 速度误差积分项 */
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s->velocity.error_integral += (float)(s->velocity.error * dt);
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// if(std::fabs(smc.error.v_error_integral) > smc.error.v_error_integral_max) //积分限幅
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// {
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// smc.error.v_error_integral = smc.error.v_error_integral_max;
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// }
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s->velocity.tar_last = s->velocity.tar_now;
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}
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//void SMC_Integval_Reset()
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//{
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// smc.error.v_error_integral = 0;
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// smc.error.p_error_integral = 0;
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//}
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/**
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* @brief 滑膜计算
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*
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* @param Sliding s结构体
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* @param mode 滑膜模式
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* @return u 输出电流
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*/
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float Smc_Calc(Sliding *s){
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/* 输出，滑模面 */
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float u,fun;
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/* tfsmc 位置 幂 (这个是移值的，放在这待开发)*/
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static float pos_pow;
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/* 力矩 */
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s->fun=fun;
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switch (s->mode) {
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case EXPONENT:///线性滑模面，指数趋近率
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if (fabs(s->position.error) - s->position.error_eps < 0){
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s->position.error = 0;
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return 0;
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}
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/* 建立滑模面 */
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s->s = s->param->c * s->position.error + s->velocity.error;
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/* 饱和函数消除抖动 */
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fun = Sat(s->s,s);
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// u = smc.param.J * ( (-smc.param.c * smc.error.v_error) - smc.param.K * smc.s - smc.param.epsilon * fun + smc.error.tar_differential_second); //控制器计算,指数趋近率
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/* 控制器计算,指数趋近率 */
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u = s->param->J * ( (-s->param->c * s->velocity.error) - s->param->K * s->s - s->param->epsilon * fun);
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s->s1=-s->param->c * s->velocity.error;
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s->s2=s->param->K * s->s;
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s->s3=s->param->epsilon * fun;
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s->s4=fun;
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break;
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case POWER:///线性滑模面，幂次趋近率
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if (fabs(s->position.error) - s->position.error_eps < 0){
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s->position.error = 0;
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return 0;
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}
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s->s = s->param->c * s->position.error + s->velocity.error; //滑模面
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fun = Sat(s->s,s);//饱和函数消除抖动
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// u = smc.param.J * ( (-smc.param.c * smc.error.v_error) - smc.param.K * smc.s - smc.param.K * (std::pow(std::fabs(smc.s),smc.param.epsilon)) * fun + smc.error.tar_differential_second); //控制器计算,幂次趋近率
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u = s->J * ( (-s->param->c * s->velocity.error) - s->param->K * s->s - s->param->K * (pow(fabs(s->s),s->param->epsilon)) * fun); //控制器计算,幂次趋近率
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break;
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case TFSMC:///tfsmc
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if (fabs(s->position.error) - s->position.error_eps < 0){
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s->position.error = 0;
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return 0;
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}
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pos_pow = pow(fabs(s->position.error),s->param->q/s->param->p);
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if(s->position.error<=0) pos_pow = -pos_pow;
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s->s = s->param->beta * pos_pow + s->velocity.error; //滑模面
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/* 饱和函数消除抖动 */
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fun = Sat(s->s,s);
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if(s->position.error!=0){
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u = s->J * (s->position.tar_differential_second//目标值的二阶导 暂定是否删除，需测试
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-s->param->K * s->s //s*K
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-s->param->epsilon * fun //epsilon*SAT(S)
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-s->velocity.error * ((s->param->q * s->param->beta) * pos_pow) / (s->param->p * s->position.error)); //控制器计算
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}
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else u = 0;
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break;
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case VELSMC:///比例积分滑模面，指数趋近律，速度控制
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/* 滑模面 */
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s->s = s->velocity.error + s->param->c * s->velocity.error_integral;
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fun = Sat(s->s,s);
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/*控制器计算，速度控制*/
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u = s->J * (s->velocity.tar_differential - (s->param->c * s->velocity.error) - s->param->K * s->s - s->param->epsilon * fun);
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break;
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case EISMC:///比例积分滑模面，指数趋近律，位置控制
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if (fabs(s->position.error) - s->position.error_eps < 0){
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s->position.error = 0;
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return 0;
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}
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/* 滑模面 */
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s->s = s->param->c1 * s->position.error + s->velocity.error + s->param->c2 * s->position.error_integral;
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fun = Sat(s->s,s);
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/* 控制器计算,指数趋近率 */
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u = s->J * ( (-s->param->c1 * s->velocity.error)- s->param->c2 * s->position.error - s->param->K * s->s - s->param->epsilon * fun);
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break;
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}
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/* 更新上一步的误差 */
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s->position.error_last = s->position.error;
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//控制量限幅
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if (u > s->param->u_max)
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{
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u = s->param->u_max;
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}
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if (u < -s->param->u_max)
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{
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u = -s->param->u_max;
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}
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s->u = u;
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return u;
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}
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