ardupilot/libraries/APM_Control/AP_RollController.h

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2013-05-29 20:53:02 -03:00
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#pragma once
#include <AP_AHRS/AP_AHRS.h>
#include <AP_Common/AP_Common.h>
#include <AP_Vehicle/AP_Vehicle.h>
#include "AP_AutoTune.h"
#include <DataFlash/DataFlash.h>
#include <AP_Math/AP_Math.h>
class AP_RollController {
public:
AP_RollController(AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms, DataFlash_Class &_dataflash) :
aparm(parms),
autotune(gains, AP_AutoTune::AUTOTUNE_ROLL, parms, _dataflash),
_ahrs(ahrs)
{
AP_Param::setup_object_defaults(this, var_info);
}
int32_t get_rate_out(float desired_rate, float scaler);
int32_t get_servo_out(int32_t angle_err, float scaler, bool disable_integrator);
void reset_I();
void autotune_start(void) { autotune.start(); }
void autotune_restore(void) { autotune.stop(); }
const DataFlash_Class::PID_Info& get_pid_info(void) const { return _pid_info; }
static const struct AP_Param::GroupInfo var_info[];
private:
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const AP_Vehicle::FixedWing &aparm;
AP_AutoTune::ATGains gains;
AP_AutoTune autotune;
uint32_t _last_t;
float _last_out;
DataFlash_Class::PID_Info _pid_info;
int32_t _get_rate_out(float desired_rate, float scaler, bool disable_integrator);
AP_AHRS &_ahrs;
};