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https://github.com/ArduPilot/ardupilot
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PID: ported to AP_HAL
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parent
40f254af51
commit
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@ -6,6 +6,9 @@
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#include <math.h>
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#include "PID.h"
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#include <AP_HAL.h>
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extern const AP_HAL::HAL& hal;
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const AP_Param::GroupInfo PID::var_info[] PROGMEM = {
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AP_GROUPINFO("P", 0, PID, _kp, 0),
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@ -15,10 +18,9 @@ const AP_Param::GroupInfo PID::var_info[] PROGMEM = {
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AP_GROUPEND
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};
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int32_t
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PID::get_pid(int32_t error, float scaler)
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int32_t PID::get_pid(int32_t error, float scaler)
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{
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uint32_t tnow = millis();
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uint32_t tnow = hal.scheduler->millis();
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uint32_t dt = tnow - _last_t;
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float output = 0;
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float delta_time;
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@ -57,7 +59,8 @@ PID::get_pid(int32_t error, float scaler)
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// high frequency noise that can drive the controller crazy
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float RC = 1/(2*M_PI*_fCut);
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derivative = _last_derivative +
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(delta_time / (RC + delta_time)) * (derivative - _last_derivative);
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((delta_time / (RC + delta_time)) *
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(derivative - _last_derivative));
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// update state
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_last_error = error;
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@ -3,11 +3,12 @@
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/// @file PID.h
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/// @brief Generic PID algorithm, with EEPROM-backed storage of constants.
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#ifndef PID_h
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#define PID_h
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#ifndef __PID_H__
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#define __PID_H__
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#include <AP_Common.h>
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#include <AP_Param.h>
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#include <stdlib.h>
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#include <math.h> // for fabs()
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/// @class PID
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@ -105,10 +106,10 @@ private:
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AP_Float _kd;
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AP_Int16 _imax;
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float _integrator; ///< integrator value
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int32_t _last_error; ///< last error for derivative
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float _last_derivative; ///< last derivative for low-pass filter
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uint32_t _last_t; ///< last time get_pid() was called in millis
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float _integrator;///< integrator value
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int32_t _last_error;///< last error for derivative
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float _last_derivative;///< last derivative for low-pass filter
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uint32_t _last_t;///< last time get_pid() was called in millis
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int32_t _get_pid(int32_t error, uint16_t dt, float scaler);
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0
libraries/PID/examples/pid/Arduino.h
Normal file
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libraries/PID/examples/pid/Arduino.h
Normal file
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libraries/PID/examples/pid/nocore.inoflag
Normal file
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libraries/PID/examples/pid/nocore.inoflag
Normal file
@ -3,37 +3,32 @@
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* 2010 Code by Jason Short. DIYDrones.com
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*/
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#include <FastSerial.h>
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#include <avr/pgmspace.h>
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#include <AP_HAL.h>
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#include <AP_Common.h>
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#include <AP_Progmem.h>
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#include <AP_Param.h>
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#include <AP_Math.h>
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#include <APM_RC.h> // ArduPilot RC Library
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#include <PID.h> // ArduPilot Mega RC Library
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#include <Arduino_Mega_ISR_Registry.h>
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#include <AP_HAL_AVR.h>
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#if CONFIG_APM_HARDWARE == APM_HARDWARE_APM2
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const AP_HAL::HAL& hal = AP_HAL_AVR_APM2;
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#else
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const AP_HAL::HAL& hal = AP_HAL_AVR_APM1;
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#endif
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long radio_in;
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long radio_trim;
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Arduino_Mega_ISR_Registry isr_registry;
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#if CONFIG_APM_HARDWARE == APM_HARDWARE_APM2
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APM_RC_APM2 APM_RC;
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#else
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APM_RC_APM1 APM_RC;
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#endif
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PID pid;
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void setup()
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{
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Serial.begin(38400);
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Serial.println("ArduPilot Mega PID library test");
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APM_RC.Init(&isr_registry); // APM Radio initialization
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hal.console->println("ArduPilot Mega PID library test");
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delay(1000);
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hal.scheduler->delay(1000);
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//rc.trim();
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radio_trim = APM_RC.InputCh(0);
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radio_trim = hal.rcin->read(0);
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pid.kP(1);
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pid.kI(0);
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@ -45,16 +40,20 @@ void setup()
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pid.kD(0);
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pid.imax(0);
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pid.load_gains();
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Serial.printf("P %f I %f D %f imax %f\n", pid.kP(), pid.kI(), pid.kD(), pid.imax());
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hal.console->printf_P(
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PSTR("P %f I %f D %f imax %f\n"),
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pid.kP(), pid.kI(), pid.kD(), pid.imax());
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}
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void loop()
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{
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delay(20);
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hal.scheduler->delay(20);
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//rc.read_pwm();
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long error = APM_RC.InputCh(0) - radio_trim;
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long control = pid.get_pid(error, 1);
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long error = hal.rcin->read(0) - radio_trim;
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long control= pid.get_pid(error, 1);
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Serial.print("control: ");
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Serial.println(control,DEC);
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hal.console->print("control: ");
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hal.console->println(control,DEC);
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}
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AP_HAL_MAIN();
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