acdt/users/Src/provalctrl.c

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#include "provalctrl.h"
//定义比例阀相结构体
propotion_valve pv_one;
propotion_valve pv_two;
//PID参数缓存用于EEPROM读写
float data_wr[3] = {0}; //[0,1,2] -> “Kp, Ti, Td”
float data_rd[3] = {0};
//比例阀参数初始化
void prov_init(void) //不同比例阀的初始参数可能会不一样,因此未使用结构体指针传参
{
ee_readfloats(PRO1_ADDR,data_rd,3); //读取存储在EEPROM里的PID参数
pv_one.status = PROV_HOLDING;
pv_one.tag = 1; //标签比例阀1
for(uint8_t i = 0;i < SLDW_PRES_OUT;i++)//前n个时刻的输出气压
{
pv_one.previous_pressure[i] = 0;
}
pv_one.current_pressure = 0; //当前气压Kpa
pv_one.current_percent = 0; //当前气压百分比( 0~900Kpa -> 0~100%
pv_one.target_pressure = 0; //目标气压Kpa
pv_one.target_percent = 0; //目标气压百分比( 0~900Kpa -> 0~100%
pv_one.target_current = 0; //目标值的理论电流
pv_one.current_input = 0; //当前输入电流
pv_one.input_min = 3; //输入电流下限
pv_one.input_max = 20; //输入电流上限
pv_one.ctrl_min = 4; //理论控制范围下限
pv_one.ctrl_max = 20; //理论控制范围上限
pv_one.bias = 0; //偏差 = 目标气压百分比 - 当前气压百分比
pv_one.bias_previous = 0; //前一个时刻的偏差
pv_one.bias_area = 0.5; //允许的误差范围±a(%)
pv_one.Kp = (isnan(data_rd[0]))?(0):(data_rd[0]); //比例系数NAN时视作0
pv_one.Ti = (data_rd[1] == 0)?(1000000):(data_rd[1]); //积分时间,防止分母为零
pv_one.Ing = 0; //积分输出
pv_one.Ing_max = 5000; //积分上限
pv_one.Ing_min = 0; //积分下限
pv_one.Ing_sum = 0; //偏差求和
pv_one.Td = data_rd[2]; //微分时间
pv_one.Ts = 0.05; //采样周期50ms
pv_one.Div = 0; //微分输出
pv_one.pidout = 0; //PID输出
pv_one.pidout_max = 0; //PID输出上限
pv_one.pidout_min = 0; //PID输出下限
pv_one.slow_down_flg = 0; //减速标志
// pv_one.cstep_gasin = 0.001; //逐步接近的电流步长mA,充气
// pv_one.cstep_gasout = 0.002; //逐步接近的电流步长mA,排气
// pv_one.cstep_max = 0; //逐步接近的电流范围上限
// pv_one.cstep_min = 0; //逐步接近的电流范围下限
// pv_one.cstep_wait = 0;
pv_one.pvout = ao_blf1_set; //DAC输出函数
pv_one.pvout(0); //输出0mA
/************************************************/
ee_readfloats(PRO2_ADDR,data_rd,3);
pv_two.status = PROV_HOLDING;
pv_two.tag = 2; //标签比例阀2
for(uint8_t i = 0;i < SLDW_PRES_OUT;i++)//前n个时刻的输出气压
{
pv_two.previous_pressure[i] = 0;
}
pv_two.current_pressure = 0;
pv_two.current_percent = 0;
pv_two.target_pressure = 0;
pv_two.target_percent = 0;
pv_two.target_current = 0; //目标值的理论电流
pv_two.current_input = 0;
pv_two.input_min = 3;
pv_two.input_max = 20;
pv_two.ctrl_min = 4; //理论控制范围下限
pv_two.ctrl_max = 20; //理论控制范围上限
pv_two.bias = 0;
pv_two.bias_previous = 0; //前一个时刻的偏差
pv_two.bias_area = 0.5;
pv_two.Kp = (isnan(data_rd[0]))?(0):(data_rd[0]);;
pv_two.Ti = (data_rd[1] == 0)?(1000000):(data_rd[1]); //积分时间
pv_two.Ing = 0;
pv_two.Ing_max = 5000;
pv_two.Ing_min = 0;
pv_two.Ing_sum = 0;
pv_two.Td = data_rd[2];
pv_two.Ts = 0.05; //采样周期50ms
pv_two.Div = 0;
pv_two.pidout = 0;
pv_two.pidout_max = 0;
pv_two.pidout_min = 0;
pv_two.slow_down_flg = 0;
// pv_two.cstep_gasin = 0.001; //逐步接近的电流步长mA,充气
// pv_two.cstep_gasout = 0.002; //逐步接近的电流步长mA,排气
// pv_two.cstep_max = 0;
// pv_two.cstep_min = 0;
// pv_two.cstep_wait = 0;
pv_two.pvout = ao_blf2_set;
pv_two.pvout(0);
}
//初始化自整定相关的参数
prov_adjust adj_pv1;
prov_adjust adj_pv2;
//初始化继电反馈整定参数
void prov_adj_init(prov_adjust *adj_pvx)
{
adj_pvx->adj_flag = 0; //自整定标志0空闲1整定中
for( uint8_t i = 0;i < OSCILL_TIMES;i++) //继电整定,振荡幅值,振荡周期
{
adj_pvx->relay_a[i] = 0;
adj_pvx->relay_tc[i] = 0;
}
adj_pvx->relay_d = 0.15; //继电整定,回环幅值
adj_pvx->air_source = 0; //气源单位Kpa
adj_pvx->middle_current = 0; //中间气压电流
adj_pvx->oscil_times = 0; //振荡次数
}
float out_makeup = 0.05; //输出补偿
//比例阀目标值设定,调节范围计算
void prov_set(float target_p, propotion_valve *pvx)
{
target_p = (target_p < pvx->input_max)?(target_p):(pvx->input_max); //dac输出限幅
target_p = (target_p > pvx->input_min)?(target_p):(pvx->input_min);
pvx->target_percent = (target_p - pvx->ctrl_min) / ( pvx->ctrl_max - pvx->ctrl_min )*100; //目标百分比,按照理论范围计算
pvx->target_pressure = pvx->target_percent/100*900; //Kpa, 比例阀 (4~20mA -> 0~0.9Mpa)
// switch (pvx->tag)//分段校准,不同比例阀的数据表不一样
// {
// case 1:
// {
// target_p = (prov_section_calculate(pvx->target_pressure,&adj_pv1) > 0)?(prov_section_calculate(pvx->target_pressure,&adj_pv1)):(target_p);
// target_p = (target_p < pvx->input_max)?(target_p):(pvx->input_max); //dac输出限幅
// target_p = (target_p > pvx->input_min)?(target_p):(pvx->input_min);
// }
// break;
// case 2:
// {
// target_p = (prov_section_calculate(pvx->target_pressure,&adj_pv2) > 0)?(prov_section_calculate(pvx->target_pressure,&adj_pv2)):(target_p);
// target_p = (target_p < pvx->input_max)?(target_p):(pvx->input_max); //dac输出限幅
// target_p = (target_p > pvx->input_min)?(target_p):(pvx->input_min);
// }
// break;
// default:
// break;
// }
pvx->target_current = target_p; //记录当前理论模拟输出
pvx->pidout_max = pvx->target_current*(1 + out_makeup); //pid输出调节上限
pvx->pidout_min = pvx->target_current*(1 - out_makeup); //pid输出调节下限
pvx->gas_direction = (pvx->target_current >= pvx->current_input)?(GAS_IN):(GAS_OUT); //判断即将进行充气还是排气
pvx->current_input = pvx->target_current; //理论值作为当前输出值
// pvx->cstep_max = pvx->current_input + (float)0.8; //逐步输出调节上限
// pvx->cstep_min = pvx->current_input - (float)0.8; //逐步输出调节下限
// pvx->cstep_wait = 0; //等待计数清零
pvx->slow_down_flg = 0; //减速标志清零
pvx->pvout(pvx->current_input); //dac输出
}
//分段计算达到目标气压所需的电流
float prov_section_calculate(float target_pressure, prov_adjust *adj_pvx)
{
float target_current = 0;
if(adj_pvx->table_pressure[SECTION_NUM - 1] == -1) return -1; //未经过整定
//寻找目标值所在区间,并根据区间占比计算所需输出
for(uint8_t i = 0;i < SECTION_NUM - 1;i++)
{
if( (target_pressure >= adj_pvx->table_pressure[i]) && (target_pressure < adj_pvx->table_pressure[i+1]) )
{
target_current = adj_pvx->table_current[i]+(adj_pvx->table_current[i+1] - adj_pvx->table_current[i]) \
* (target_pressure - adj_pvx->table_pressure[i])/(adj_pvx->table_pressure[i+1] - adj_pvx->table_pressure[i]); //目标气压在所在区间内的百分比
}
if(target_pressure >= adj_pvx->table_pressure[SECTION_NUM - 1]) target_current = adj_pvx->table_current[SECTION_NUM - 1];
}
return target_current;
}
//绝对值计算
float abs_bias(float bias)
{
bias =( bias>=0 )?(bias):(-bias);
return bias;
}
//pid控制
float beta_in = 0, beta_out = 0; //变速积分
void prov_calibrate_pid(propotion_valve *pvx)
{
if( (abs_bias(pvx->bias) > pvx->bias_area ) && (abs_bias(pvx->bias) < BIAS_MAX) ) //误差进入目标±BIAS_MAX%以内后再进行控制
{
//变速积分
beta_in = ( abs_bias(pvx->bias*pvx->bias) + BIAS_MAX ) / ( BIAS_MAX );
beta_out = ( abs_bias(pvx->bias) + BIAS_MAX/2 ) / ( BIAS_MAX );
//充放气过程分开处理
switch(pvx->gas_direction)
{
case GAS_IN: //充气
{
pvx->Ing_sum += pvx->bias * beta_in; //偏差求和
pvx->Ing_sum = (pvx->Ing_sum > pvx->Ing_max)?(pvx->Ing_max):(pvx->Ing_sum); //积分限幅
pvx->Ing_sum = (pvx->Ing_sum < pvx->Ing_min)?(pvx->Ing_min):(pvx->Ing_sum);
pvx->Ing = ( pvx->Ts / pvx->Ti ) * pvx->Ing_sum; //积分项
pvx->Div = ( pvx->Td / pvx->Ts ) * ( pvx->bias - pvx->bias_previous ); //微分项
pvx->pidout = pvx->Kp*( pvx->bias + pvx->Ing + pvx->Div ); //pid输出
pvx->current_input = (pvx->pidout/100) * (pvx->input_max - pvx->input_min) + pvx->input_min;
}
break;
case GAS_OUT: //排气
{
pvx->Ing_sum += pvx->bias * beta_out; //偏差求和
pvx->Ing_sum = (pvx->Ing_sum > pvx->Ing_max)?(pvx->Ing_max):(pvx->Ing_sum); //积分限幅
pvx->Ing_sum = (pvx->Ing_sum < pvx->Ing_min)?(pvx->Ing_min):(pvx->Ing_sum);
pvx->Ing = ( pvx->Ts / pvx->Ti ) * pvx->Ing_sum; //积分项
pvx->Div = ( pvx->Td / pvx->Ts ) * ( pvx->bias - pvx->bias_previous ); //微分项
pvx->pidout = pvx->Kp*( pvx->bias + pvx->Ing + pvx->Div ); //pid输出
pvx->current_input = (pvx->pidout/100) * (pvx->input_max - pvx->input_min) + pvx->input_min;
}
break;
default:
{
}
break;
}
pvx->current_input = (pvx->current_input < pvx->pidout_max)?(pvx->current_input):(pvx->pidout_max); //充气时限制输出上限
pvx->current_input = (pvx->current_input > pvx->pidout_min)?(pvx->current_input):(pvx->pidout_min); //排气时限制输出下限
pvx->bias_previous = pvx->bias; //更新前一个时刻的偏差
if( abs_bias(pvx->previous_pressure[0] - pvx->previous_pressure[SLDW_PRES_OUT - 1]) <= 10 ) //判断是否趋于稳定
{
pvx->slow_down_flg = 1;
}
pvx->current_input = (pvx->target_current < pvx->input_max*(float)(0.995))?(pvx->current_input):(pvx->input_max); //小信号切除
if( pvx->target_current <= pvx->input_min*(float)(1.005) )
{
pvx->current_input = pvx->input_min;
pvx->Ing_sum = 0;
}
pvx->pvout(pvx->current_input); //dac输出
}else if(abs_bias(pvx->bias) >= BIAS_MAX)
{
switch(pvx->gas_direction) //根据气体方向对输出范围做补偿
{
case GAS_IN:
{
pvx->Ing_sum = (pvx->target_percent - 100*out_makeup) / pvx->Kp / ( pvx->Ts / pvx->Ti ); //预估积分值,改善滞后
pvx->Ing_sum = (pvx->Ing_sum < pvx->Ing_min)?(pvx->Ing_min):(pvx->Ing_sum);
}
break;
case GAS_OUT:
{
pvx->Ing_sum = pvx->target_percent / pvx->Kp / ( pvx->Ts / pvx->Ti ); //预估积分值,改善滞后
}
break;
default:
{
}
break;
}
}
}
//模拟量控制
float ao_dwq = 0; //AO输出电流值(定位器)
float ao_blf1 = 0; //AO输出电流值(比例阀)
float ao_blf2 = 0; //AO输出电流值(比例阀)
float atm_pressure = 0; //用于存放大气绝压单位0.1Kpa
adj_steps astep = ADJ_WAIT; //自整定步骤,继电反馈
adj_section_steps astep_s = SECTION_WAIT; //自整定步骤,分段
void analog_ctrl(void)
{
if(ao_dwq != (float)(HoldReg[0]) / 1000) //保持寄存器值发生变化时dac输出
{
ao_dwq = (float)(HoldReg[0]) / 1000; // uA -> mA
if(ao_dwq > 25) ao_dwq = 25; //定位器控制
ao_dwq_set(ao_dwq);
}
if( ao_blf1!= (float)(HoldReg[1]) / 1000) //保持寄存器值发生变化时dac输出
{
ao_blf1 = (float)(HoldReg[1]) / 1000; // uA -> mA
ao_blf1_set(ao_blf1);
//prov_set(ao_blf1,&pv_one); //控制比例阀1
}
if(ao_blf2 != (float)(HoldReg[2]) / 1000) //保持寄存器值发生变化时dac输出
{
ao_blf2 = (float)(HoldReg[2]) / 1000; // uA -> mA
ao_blf2_set(ao_blf2);
//prov_set(ao_blf2,&pv_two); //控制比例阀2
}
// if( (CoilState[3]&(0x40)) == 0x40 ) //触发比例阀1自整定
// {
// if( (astep_s == SECTION_WAIT) && (pv_two.status != PROV_ADJUSTING) )
// {
// pv_one.status = PROV_ADJUSTING;
// }
// }
//
// if( (CoilState[3]&(0x20)) == 0x20 ) //触发比例阀2自整定
// {
// if( (astep_s == SECTION_WAIT) && (pv_one.status != PROV_ADJUSTING) )
// {
// pv_two.status = PROV_ADJUSTING;
// }
// }
if(it_100ms_flag_pv == 1) //每隔100ms更新一次数据
{
it_100ms_flag_pv = 0;
InputReg[7] = ( (InputReg[7]<16000)&&(InputReg[7]>8000) )?(InputReg[7]):(12000); //应对没接大气压力的情况
atm_pressure = ( (InputReg[7] - 4000)/(float)16000.0 ) * 2000; //大气绝压更新,4~20mA->0~200Kpa
for(uint8_t i = 1;i< SLDW_PRES_OUT;i++) //滑动窗口,记录历史纯输出气压
{
pv_one.previous_pressure[SLDW_PRES_OUT - i] = pv_one.previous_pressure[SLDW_PRES_OUT - i - 1];
pv_two.previous_pressure[SLDW_PRES_OUT - i] = pv_two.previous_pressure[SLDW_PRES_OUT - i - 1];
}
pv_one.previous_pressure[0] = pv_one.current_pressure;
pv_two.previous_pressure[0] = pv_two.current_pressure;
//比例阀1数据更新当前气压、当前气压百分比、百分比偏差、当前输入电流单片机->比例阀)
pv_one.current_pressure = (InputReg[16] - atm_pressure)/(float)10; //Kpasensor1 A口绝压转表压
pv_one.current_percent = pv_one.current_pressure/900*100;
pv_one.bias = pv_one.target_percent - pv_one.current_percent;
//比例阀2数据更新当前气压、当前气压百分比、百分比偏差、当前输入电流单片机->比例阀)
pv_two.current_pressure = (InputReg[17] - atm_pressure)/(float)10; //Kpasensor1 B口绝压转表压
pv_two.current_percent = pv_two.current_pressure/900*100;
pv_two.bias = pv_two.target_percent - pv_two.current_percent;
}
// if(it_50ms_flag_pv == 1) //每隔50ms校准一次
// {
// it_50ms_flag_pv = 0;
//
// //每个比例阀对应两个电磁阀,一个是气源一个是锁止阀
// if( (CoilState[0]&(0x03)) == 0x03 ) //2个电磁阀都开启的情况下才进行控制比例阀1,否则保持
// {
// if(pv_two.status != PROV_ADJUSTING) //对其中一个比例阀进行自整定时,不对另一个进行控制
// {
// prov_ctrl(&pv_one, &adj_pv1);
// }
// }
//
// if( (CoilState[0]&(0x0C)) == 0x0C ) //2个电磁阀都开启的情况下才进行控制比例阀2,否则保持
// {
// if(pv_one.status != PROV_ADJUSTING) //对其中一个比例阀进行自整定时,不对另一个进行控制
// {
// prov_ctrl(&pv_two, &adj_pv2);
// }
// }
// }
}
//比例阀控制
void prov_ctrl(propotion_valve *pvx, prov_adjust *adj_pvx)
{
switch(pvx->status)
{
case PROV_RUNNING: //介入控制
{
if(adj_pvx->adj_flag == 1) //进入此处说明整定被打断
{
//整定结束
prov_adj_init(adj_pvx);
astep = ADJ_WAIT;
astep_s = SECTION_WAIT;
}
// prov_calibrate_step(&pvx);
prov_calibrate_pid(pvx);
}
break;
case PROV_ADJUSTING: //自整定
{
// //继电反馈
// if(astep == ADJ_WAIT)
// {
// prov_adj_init(adj_pvx);
// adj_pvx->adj_flag = 1; //整定开始
// astep = ADJ_START;
// }
// prov_adj(pvx, adj_pvx);
//分段
if(astep_s == SECTION_WAIT)
{
prov_adj_section_init(adj_pvx);
adj_pvx->adj_flag = 1; //整定开始
astep_s = SECTION_START;
}
prov_adj_section(pvx, adj_pvx);
}
break;
case PROV_HOLDING: //保持原样,不介入控制
{
if(adj_pvx->adj_flag == 1) //进入此处说明整定被打断
{
//整定结束
prov_adj_init(adj_pvx);
astep = ADJ_WAIT;
astep_s = SECTION_WAIT;
}
}
break;
default:
{
return;
}
}
}
int tick_previous = -1; //用于计时
int tick_current = -1;
uint8_t hys_flag = 0; //0:充气, 1:排气
//PID参数自整定继电反馈
void prov_adj(propotion_valve *pvx, prov_adjust *adj_pvx)
{
switch(astep)
{
case ADJ_START:
{
if(tick_previous == -1)
{
tick_previous = tick500ms;
prov_set(4,pvx);//排空气体
}
tick_current = tick500ms;
if( (tick_current - tick_previous) > 20) //等待20*500ms
{
//记录此时气源压力
adj_pvx->air_source = (InputReg[18] - atm_pressure) / (float)10;
tick_previous = -1;
tick_current = -1;
astep++;
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
}
break;
case ADJ_MOVE2MIDDLE:
{
if(tick_previous == -1)
{
tick_previous = tick500ms;
//输出气源50%压力,根据目标压力倒推所需电流值
adj_pvx->middle_current = (adj_pvx->air_source/2/900)*(pvx->input_max - pvx->input_min) + pvx->input_min;
adj_pvx->middle_current = (adj_pvx->middle_current < pvx->input_max)?(adj_pvx->middle_current):(pvx->input_max); //dac输出限幅
adj_pvx->middle_current = (adj_pvx->middle_current > pvx->input_min)?(adj_pvx->middle_current):(pvx->input_min);
prov_set(adj_pvx->middle_current,pvx);
}
tick_current = tick500ms;
if( (tick_current - tick_previous) > 10) //等待10*500ms
{
tick_previous = -1;
tick_current = -1;
astep++;
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
}
break;
case ADJ_OSCILLATE:
{
if(adj_pvx->oscil_times < OSCILL_TIMES) //振荡次数是否达到目标
{
if(tick_previous == -1) //计时开始,记录起始时间
{
tick_previous = tick500ms;
}else
{
//记录第 oc_times 个周期的峰值
adj_pvx->relay_a[adj_pvx->oscil_times] = (adj_pvx->relay_a[adj_pvx->oscil_times] < pvx->current_pressure)?(pvx->current_pressure):(adj_pvx->relay_a[adj_pvx->oscil_times]);
}
tick_current = tick500ms; //记录当前时间
if( (tick_current - tick_previous) > TICK_LIMIT ) //是否超时TICK_LIMIT*500ms
{
astep = ADJ_END; //强制打断
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
if( ( pvx->current_pressure < (adj_pvx->air_source/2*(1 + adj_pvx->relay_d)) ) && (hys_flag == 0) ) //充气振荡
{
pvx->current_input = adj_pvx->middle_current*(1 + adj_pvx->relay_d); //输出气源 50*(1+d)% 压力
pvx->current_input = (pvx->current_input < pvx->input_max)?(pvx->current_input):(pvx->input_max); //dac输出限幅
pvx->current_input = (pvx->current_input > pvx->input_min)?(pvx->current_input):(pvx->input_min);
prov_set(pvx->current_input,pvx);
}else if( pvx->current_pressure >= (adj_pvx->air_source/2*(1 + adj_pvx->relay_d)) && (hys_flag == 0)) //切换至排气
{
hys_flag = 1;
}
if( ( pvx->current_pressure > (adj_pvx->air_source/2*(1 - adj_pvx->relay_d)) ) && (hys_flag == 1) ) //排气振荡
{
pvx->current_input = adj_pvx->middle_current*(1 - adj_pvx->relay_d); //输出气源 50*(1-d)% 压力
pvx->current_input = (pvx->current_input < pvx->input_max)?(pvx->current_input):(pvx->input_max); //dac输出限幅
pvx->current_input = (pvx->current_input > pvx->input_min)?(pvx->current_input):(pvx->input_min);
prov_set(pvx->current_input,pvx);
}else if( pvx->current_pressure <= (adj_pvx->air_source/2*(1 - adj_pvx->relay_d)) && (hys_flag == 1) ) //切换至充气
{
hys_flag = 0;
adj_pvx->relay_tc[adj_pvx->oscil_times] = (tick_current - tick_previous) * 500; //振荡周期单位ms
tick_previous = -1; //重新开始计时
tick_current = -1;
adj_pvx->oscil_times++; //开始下一次振荡
}
}else //振荡次数达到目标
{
if(tick_previous == -1)
{
tick_previous = tick500ms;
}
tick_current = tick500ms;
if( (tick_current - tick_previous) > 6) //等待6*500ms后排气
{
prov_set(4,pvx);
tick_previous = -1;
tick_current = -1;
astep++;
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
}
}
break;
case ADJ_CALCULATE:
{
for(uint8_t i = 0;i < OSCILL_TIMES; i++) //对振荡周期和峰值作均值滤波
{
adj_pvx->relay_A += adj_pvx->relay_a[i];
adj_pvx->relay_Tc += adj_pvx->relay_tc[i];
}
adj_pvx->relay_A /= OSCILL_TIMES * ( adj_pvx->air_source/2 * (1 + adj_pvx->relay_d) );
adj_pvx->relay_Tc /= OSCILL_TIMES;
/* PI [0.45,0.8]*/
/* PID [0.6,0.5,0.12]*/
pvx->Kp = (float)0.6 * ( 4 * (float)0.1 ) / ( (float)3.1415 * adj_pvx->relay_A ) / 3;
pvx->Ti = (float)0.5 * adj_pvx->relay_Tc/1000 / 20;
pvx->Td = (float)0.12 * adj_pvx->relay_Tc/1000;
pvx->Ing_sum = 0;
switch(pvx->tag)
{
case 1:
{
data_wr[0] = pvx->Kp;
data_wr[1] = pvx->Ti;
data_wr[2] = pvx->Td;
ee_writefloats(PRO1_ADDR,data_wr,3);
}
break;
case 2:
{
data_wr[0] = pvx->Kp;
data_wr[1] = pvx->Ti;
data_wr[2] = pvx->Td;
ee_writefloats(PRO2_ADDR,data_wr,3);
}
break;
default:
{
}
break;
}
astep++;
}
break;
case ADJ_END:
{
if(tick_previous == -1)
{
tick_previous = tick500ms;
}
tick_current = tick500ms;
if( (tick_current - tick_previous) > 10) //等待10*500ms后恢复控制等待期间排气 + 计算结果)
{
switch(pvx->tag) //重新触发保持寄存器
{
case 1:
{
ao_blf1 = -1;
CoilState[3] &= 0xBF; //D6 = 0, [1011 1111]
}
break;
case 2:
{
ao_blf2 = -1;
CoilState[3] &= 0xDF; //D5 = 0, [1101 1111]
}
break;
default:
{
}
break;
}
tick_previous = -1;
tick_current = -1;
prov_adj_init(adj_pvx);
pvx->status = PROV_RUNNING; //恢复控制
astep++;
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
}
break;
case ADJ_WAIT:
{
}
break;
default:
{
return;
}
}
}
//分段校准参数初始化
void prov_adj_section_init(prov_adjust *adj_pvx)
{
adj_pvx->adj_flag = 0;
adj_pvx->stable_area = 9;
adj_pvx->wait_tick = 2 * 30;
for(uint8_t i = 0; i < SECTION_NUM; i++)
{
adj_pvx->table_current[i] = -1;
adj_pvx->table_pressure[i] = -1;
}
}
uint8_t temp_cnt = 0;
//分段校准
void prov_adj_section(propotion_valve *pvx, prov_adjust *adj_pvx)
{
switch (astep_s)
{
case SECTION_START:
{
if(tick_previous == -1)
{
tick_previous = tick500ms;
prov_set(pvx->input_min,pvx); //排空气体
}
tick_current = tick500ms;
if( (tick_current - tick_previous) > 20) //等待20*500ms
{
tick_previous = -1;
tick_current = -1;
astep_s++;
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
}
break;
case SECTION_RECORD_AIRSOURCE:
{
//记录此时气源压力
adj_pvx->air_source = (InputReg[18] - atm_pressure) / (float)10;
//计算分段电流,上限为气源倒推得到的电流值
adj_pvx->table_current[SECTION_NUM-1] = adj_pvx->air_source/900 * (pvx->ctrl_max - pvx->ctrl_min) + pvx->ctrl_min;
for(uint8_t i = 0;i < SECTION_NUM - 1;i++)
{
adj_pvx->table_current[i] = pvx->ctrl_min + i * (adj_pvx->table_current[SECTION_NUM-1] - pvx->ctrl_min)/(SECTION_NUM - 1);
}
astep_s++;
}
break;
case SECTION_MOVE:
{
if(tick_previous == -1)
{
tick_previous = tick500ms;
prov_set( adj_pvx->table_current[temp_cnt], pvx ); //设定分段电流
}
tick_current = tick500ms;
if( (tick_current - tick_previous) > adj_pvx->wait_tick) //等待tick*500ms
{
adj_pvx->table_pressure[temp_cnt] = pvx->current_pressure; //记录当前实际气压
tick_previous = -1; //准备下一次计时
tick_current = -1;
temp_cnt++; //下一个
if(temp_cnt >= SECTION_NUM)
{
temp_cnt = 0;
astep_s++;
}
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
}
break;
case SECTION_END:
{
if(tick_previous == -1)
{
tick_previous = tick500ms;
}
tick_current = tick500ms;
if( (tick_current - tick_previous) > 10) //等待10*500ms后恢复控制等待期间排气 + 计算结果)
{
switch(pvx->tag) //重新触发保持寄存器
{
case 1:
{
ao_blf1 = -1;
CoilState[3] &= 0xBF; //D6 = 0, [1011 1111]
}
break;
case 2:
{
ao_blf2 = -1;
CoilState[3] &= 0xDF; //D5 = 0, [1101 1111]
}
break;
default:
{
}
break;
}
tick_previous = -1;
tick_current = -1;
adj_pvx->adj_flag = 0;
pvx->status = PROV_HOLDING; //恢复控制
astep_s++;
}else if( (tick_current - tick_previous) < 0)
{
tick_previous = -1;
tick_current = -1;
}
}
break;
case SECTION_WAIT:
{
}
break;
default:
break;
}
}