#include <mode.h>

Inheritance diagram for ModeAcro_Heli:

Public Member Functions
bool	init (bool ignore_checks) override

void	run () override

Public Member Functions inherited from ModeAcro
bool	is_autopilot () const override

bool	requires_GPS () const override

bool	has_manual_throttle () const override

bool	allows_arming (bool from_gcs) const override

Additional Inherited Members
Static Public Attributes inherited from Mode
static AutoYaw	auto_yaw

Protected Member Functions inherited from ModeAcro
const char *	name () const override

const char *	name4 () const override

void	get_pilot_desired_angle_rates (int16_t roll_in, int16_t pitch_in, int16_t yaw_in, float &roll_out, float &pitch_out, float &yaw_out)

Protected Member Functions inherited from Mode
virtual bool	landing_gear_should_be_deployed () const

void	update_navigation ()

virtual void	run_autopilot ()

virtual uint32_t	wp_distance () const

virtual int32_t	wp_bearing () const

virtual bool	get_wp (Location_Class &loc)

virtual bool	in_guided_mode () const

void	get_pilot_desired_lean_angles (float &roll_out, float &pitch_out, float angle_max, float angle_limit) const

bool	takeoff_triggered (float target_climb_rate) const

void	zero_throttle_and_relax_ac ()

int32_t	get_alt_above_ground (void)

void	land_run_horizontal_control ()

void	land_run_vertical_control (bool pause_descent=false)

float	get_surface_tracking_climb_rate (int16_t target_rate, float current_alt_target, float dt)

float	get_pilot_desired_yaw_rate (int16_t stick_angle)

float	get_pilot_desired_climb_rate (float throttle_control)

float	get_pilot_desired_throttle (int16_t throttle_control, float thr_mid=0.0f)

float	get_non_takeoff_throttle (void)

void	update_simple_mode (void)

bool	set_mode (control_mode_t mode, mode_reason_t reason)

void	set_land_complete (bool b)

GCS_Copter &	gcs ()

void	Log_Write_Event (uint8_t id)

void	set_throttle_takeoff (void)

void	takeoff_timer_start (float alt_cm)

void	takeoff_stop (void)

void	takeoff_get_climb_rates (float &pilot_climb_rate, float &takeoff_climb_rate)

float	get_avoidance_adjusted_climbrate (float target_rate)

uint16_t	get_pilot_speed_dn (void)

Protected Attributes inherited from Mode
Parameters &	g

ParametersG2 &	g2

AC_WPNav *&	wp_nav

AC_Loiter *&	loiter_nav

AC_PosControl *&	pos_control

AP_InertialNav &	inertial_nav

AP_AHRS &	ahrs

AC_AttitudeControl_t *&	attitude_control

MOTOR_CLASS *&	motors

RC_Channel *&	channel_roll

RC_Channel *&	channel_pitch

RC_Channel *&	channel_throttle

RC_Channel *&	channel_yaw

float &	G_Dt

ap_t &	ap

takeoff_state_t &	takeoff_state

float &	ekfGndSpdLimit

float &	ekfNavVelGainScaler

heli_flags_t &	heli_flags

Member Function Documentation

◆ init()

bool ModeAcro_Heli::init ( bool ignore_checks )

overridevirtual

Reimplemented from ModeAcro.

◆ run()

void ModeAcro_Heli::run ( )

overridevirtual

Reimplemented from ModeAcro.

The documentation for this class was generated from the following file:

C:/GitHub/ardupilot/ArduCopter/mode.h

Public Member Functions

Additional Inherited Members

Member Function Documentation

◆ init()

◆ run()