#include <mode.h>
Inheritance diagram for ModeAcro:
Collaboration diagram for ModeAcro:
Public Member Functions | |
| virtual bool | init (bool ignore_checks) override |
| virtual void | run () override |
| bool | is_autopilot () const override |
| bool | requires_GPS () const override |
| bool | has_manual_throttle () const override |
| bool | allows_arming (bool from_gcs) const override |
Protected Member Functions | |
| 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) |
Additional Inherited Members | |
| Static Public Attributes inherited from Mode | |
| static AutoYaw | auto_yaw |
| 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 |
Detailed Description
Member Function Documentation
◆ allows_arming()
|
inlineoverridevirtual |
◆ get_pilot_desired_angle_rates()
|
protected |
◆ has_manual_throttle()
|
inlineoverridevirtual |
◆ init()
|
overridevirtual |
Implements Mode.
Reimplemented in ModeAcro_Heli.
◆ is_autopilot()
|
inlineoverridevirtual |
◆ name()
|
inlineoverrideprotectedvirtual |
◆ name4()
|
inlineoverrideprotectedvirtual |
◆ requires_GPS()
|
inlineoverridevirtual |
◆ run()
|
overridevirtual |
Implements Mode.
Reimplemented in ModeAcro_Heli.
The documentation for this class was generated from the following file:
- ArduCopter/mode.h
