// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*-
/// @file AC_AttitudeControl_Heli.h
/// @brief ArduCopter attitude control library for traditional helicopters
# ifndef AC_ATTITUDECONTROL_HELI_H
# define AC_ATTITUDECONTROL_HELI_H
# include <AC_AttitudeControl.h>
# include <AC_HELI_PID.h>
# include <Filter.h>
# define AC_ATTITUDE_HELI_RATE_INTEGRATOR_LEAK_RATE 0.02f
# define AC_ATTITUDE_HELI_RATE_RP_FF_FILTER 10.0f
# define AC_ATTITUDE_HELI_RATE_Y_VFF_FILTER 10.0f
# define AC_ATTITUDE_HELI_RATE_Y_AFF_FILTER 10.0f
class AC_AttitudeControl_Heli : public AC_AttitudeControl {
public :
AC_AttitudeControl_Heli ( AP_AHRS & ahrs ,
const AP_Vehicle : : MultiCopter & aparm ,
AP_MotorsHeli & motors ,
AC_P & p_angle_roll , AC_P & p_angle_pitch , AC_P & p_angle_yaw ,
AC_HELI_PID & pid_rate_roll , AC_HELI_PID & pid_rate_pitch , AC_HELI_PID & pid_rate_yaw
) :
AC_AttitudeControl ( ahrs , aparm , motors ,
p_angle_roll , p_angle_pitch , p_angle_yaw ,
pid_rate_roll , pid_rate_pitch , pid_rate_yaw ) ,
_passthrough_roll ( 0 ) , _passthrough_pitch ( 0 ) ,
pitch_feedforward_filter ( AC_ATTITUDE_HELI_RATE_RP_FF_FILTER ) ,
roll_feedforward_filter ( AC_ATTITUDE_HELI_RATE_RP_FF_FILTER ) ,
yaw_velocity_feedforward_filter ( AC_ATTITUDE_HELI_RATE_Y_VFF_FILTER ) ,
yaw_acceleration_feedforward_filter ( AC_ATTITUDE_HELI_RATE_Y_AFF_FILTER )
{
AP_Param : : setup_object_defaults ( this , var_info ) ;
}
// passthrough_bf_roll_pitch_rate_yaw - roll and pitch are passed through directly, body-frame rate target for yaw
void passthrough_bf_roll_pitch_rate_yaw ( float roll_passthrough , float pitch_passthrough , float yaw_rate_bf ) ;
// rate_controller_run - run lowest level body-frame rate controller and send outputs to the motors
// should be called at 100hz or more
virtual void rate_controller_run ( ) ;
// use_leaky_i - controls whether we use leaky i term for body-frame to motor output stage
void use_leaky_i ( bool leaky_i ) { _flags_heli . leaky_i = leaky_i ; }
// use_flybar_passthrough - controls whether we pass-through control inputs to swash-plate
void use_flybar_passthrough ( bool passthrough ) { _flags_heli . flybar_passthrough = passthrough ; }
// user settable parameters
static const struct AP_Param : : GroupInfo var_info [ ] ;
private :
// To-Do: move these limits flags into the heli motors class
struct AttControlHeliFlags {
uint8_t limit_roll : 1 ; // 1 if we have requested larger roll angle than swash can physically move
uint8_t limit_pitch : 1 ; // 1 if we have requested larger pitch angle than swash can physically move
uint8_t limit_yaw : 1 ; // 1 if we have requested larger yaw angle than tail servo can physically move
uint8_t leaky_i : 1 ; // 1 if we should use leaky i term for body-frame rate to motor stage
uint8_t flybar_passthrough : 1 ; // 1 if we should pass through pilots roll & pitch input directly to swash-plate
} _flags_heli ;
//
// body-frame rate controller
//
// rate_bf_to_motor_roll_pitch - ask the rate controller to calculate the motor outputs to achieve the target body-frame rate (in centi-degrees/sec) for roll, pitch and yaw
// outputs are sent directly to motor class
void rate_bf_to_motor_roll_pitch ( float rate_roll_target_cds , float rate_pitch_target_cds ) ;
virtual float rate_bf_to_motor_yaw ( float rate_yaw_cds ) ;
//
// throttle methods
//
// calculate total body frame throttle required to produce the given earth frame throttle
float get_boosted_throttle ( float throttle_in ) ;
// pass through for roll and pitch
int16_t _passthrough_roll ;
int16_t _passthrough_pitch ;
// LPF filters to act on Rate Feedforward terms to linearize output.
// Due to complicated aerodynamic effects, feedforwards acting too fast can lead
// to jerks on rate change requests.
LowPassFilterFloat pitch_feedforward_filter ;
LowPassFilterFloat roll_feedforward_filter ;
LowPassFilterFloat yaw_velocity_feedforward_filter ;
LowPassFilterFloat yaw_acceleration_feedforward_filter ;
} ;
# endif //AC_ATTITUDECONTROL_HELI_H