// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #pragma once #include #include #include #include "AP_AutoTune.h" #include #include class AP_RollController { public: AP_RollController(AP_Airspeed &aspeed, AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms, DataFlash_Class &_dataflash) : airspeed(aspeed), 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[]; // tuning accessors void kP(float v) { gains.P.set(v); } void kI(float v) { gains.I.set(v); } void kD(float v) { gains.D.set(v); } void kFF(float v) { gains.FF.set(v); } AP_Float &kP(void) { return gains.P; } AP_Float &kI(void) { return gains.I; } AP_Float &kD(void) { return gains.D; } AP_Float &kFF(void) { return gains.FF; } private: const AP_Vehicle::FixedWing &aparm; const AP_Airspeed &airspeed; 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; };