ArduCopter
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#include <mode.h>
Public Member Functions | |
bool | init (bool ignore_checks) override |
void | run () override |
bool | requires_GPS () const override |
bool | has_manual_throttle () const override |
bool | allows_arming (bool from_gcs) const override |
bool | is_autopilot () const override |
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bool | in_guided_mode () const |
void | set_angle (const Quaternion &q, float climb_rate_cms, bool use_yaw_rate, float yaw_rate_rads) |
bool | set_destination (const Vector3f &destination, bool use_yaw=false, float yaw_cd=0.0, bool use_yaw_rate=false, float yaw_rate_cds=0.0, bool yaw_relative=false) |
bool | set_destination (const Location_Class &dest_loc, bool use_yaw=false, float yaw_cd=0.0, bool use_yaw_rate=false, float yaw_rate_cds=0.0, bool yaw_relative=false) |
bool | get_wp (Location_Class &loc) override |
void | set_velocity (const Vector3f &velocity, bool use_yaw=false, float yaw_cd=0.0, bool use_yaw_rate=false, float yaw_rate_cds=0.0, bool yaw_relative=false, bool log_request=true) |
bool | set_destination_posvel (const Vector3f &destination, const Vector3f &velocity, bool use_yaw=false, float yaw_cd=0.0, bool use_yaw_rate=false, float yaw_rate_cds=0.0, bool yaw_relative=false) |
void | limit_clear () |
void | limit_init_time_and_pos () |
void | limit_set (uint32_t timeout_ms, float alt_min_cm, float alt_max_cm, float horiz_max_cm) |
bool | limit_check () |
bool | takeoff_start (float final_alt_above_home) |
GuidedMode | mode () const |
void | angle_control_start () |
void | angle_control_run () |
Protected Member Functions | |
const char * | name () const override |
const char * | name4 () const override |
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uint32_t | wp_distance () const override |
int32_t | wp_bearing () const override |
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virtual bool | landing_gear_should_be_deployed () const |
void | update_navigation () |
virtual void | run_autopilot () |
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 | |
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static AutoYaw | auto_yaw |
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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 |
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inlineoverridevirtual |
Reimplemented from ModeGuided.
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inlineoverridevirtual |
Reimplemented from ModeGuided.
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overridevirtual |
Reimplemented from ModeGuided.
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inlineoverridevirtual |
Reimplemented from ModeGuided.
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inlineoverrideprotectedvirtual |
Reimplemented from ModeGuided.
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inlineoverrideprotectedvirtual |
Reimplemented from ModeGuided.
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inlineoverridevirtual |
Reimplemented from ModeGuided.
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overridevirtual |
Reimplemented from ModeGuided.