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- #pragma once
- #include <AP_AHRS/AP_AHRS.h>
- #include <AP_Common/AP_Common.h>
- #include <AP_Vehicle/AP_Vehicle.h>
- #include <AP_Logger/AP_Logger.h>
- #include <cmath>
- class AP_YawController {
- public:
- AP_YawController(AP_AHRS &ahrs, const AP_Vehicle::FixedWing &parms)
- : aparm(parms)
- , _ahrs(ahrs)
- {
- AP_Param::setup_object_defaults(this, var_info);
- _pid_info.target = 0;
- _pid_info.FF = 0;
- _pid_info.P = 0;
- }
- /* Do not allow copies */
- AP_YawController(const AP_YawController &other) = delete;
- AP_YawController &operator=(const AP_YawController&) = delete;
- int32_t get_servo_out(float scaler, bool disable_integrator);
- void reset_I();
- /*
- reduce the integrator, used when we have a low scale factor in a quadplane hover
- */
- void decay_I() {
- // this reduces integrator by 95% over 2s
- _pid_info.I *= 0.995f;
- }
-
- const AP_Logger::PID_Info& get_pid_info(void) const {return _pid_info; }
- static const struct AP_Param::GroupInfo var_info[];
- private:
- const AP_Vehicle::FixedWing &aparm;
- AP_Float _K_A;
- AP_Float _K_I;
- AP_Float _K_D;
- AP_Float _K_FF;
- AP_Int16 _imax;
- uint32_t _last_t;
- float _last_out;
- float _last_rate_hp_out;
- float _last_rate_hp_in;
- float _K_D_last;
- float _integrator;
- AP_Logger::PID_Info _pid_info;
- AP_AHRS &_ahrs;
- };
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