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APM:Copter
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Public Member Functions | |
| ModeFlowHold (void) | |
| bool | init (bool ignore_checks) override |
| void | run (void) 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 |
Static Public Attributes | |
| static const struct AP_Param::GroupInfo | var_info [] |
Static Public Attributes inherited from Copter::Mode | |
| static AutoYaw | auto_yaw |
Protected Member Functions | |
| const char * | name () const override |
| const char * | name4 () const override |
Protected Member Functions inherited from Copter::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) |
Private Types | |
| enum | FlowHoldModeState { FlowHold_MotorStopped, FlowHold_Takeoff, FlowHold_Flying, FlowHold_Landed } |
Private Member Functions | |
| void | flow_to_angle (Vector2f &bf_angle) |
| bool | flowhold_init (bool ignore_checks) |
| void | flowhold_run () |
| void | flowhold_flow_to_angle (Vector2f &angle, bool stick_input) |
| void | update_height_estimate (void) |
Private Attributes | |
| LowPassFilterVector2f | flow_filter |
| const float | height_min = 0.1 |
| const float | height_max = 3.0 |
| AP_Float | flow_max |
| AC_PI_2D | flow_pi_xy {0.2, 0.3, 3000, 5, 0.0025} |
| AP_Float | flow_filter_hz |
| AP_Int8 | flow_min_quality |
| AP_Int8 | brake_rate_dps |
| float | quality_filtered |
| uint8_t | log_counter |
| bool | limited |
| Vector2f | xy_I |
| Vector2f | delta_velocity_ne |
| Vector2f | last_flow_rate_rps |
| uint32_t | last_flow_ms |
| float | last_ins_height |
| float | height_offset |
| bool | braking |
| uint32_t | last_stick_input_ms |
Additional Inherited Members | |
Protected Attributes inherited from Copter::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 |
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private |
| Copter::ModeFlowHold::ModeFlowHold | ( | void | ) |
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inlineoverridevirtual |
Implements Copter::Mode.
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private |
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private |
Definition at line 119 of file mode_flowhold.cpp.
Referenced by run().
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private |
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inlineoverridevirtual |
Implements Copter::Mode.
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overridevirtual |
Implements Copter::Mode.
Definition at line 78 of file mode_flowhold.cpp.
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inlineoverridevirtual |
Reimplemented from Copter::Mode.
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inlineoverrideprotectedvirtual |
Implements Copter::Mode.
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inlineoverrideprotectedvirtual |
Implements Copter::Mode.
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inlineoverridevirtual |
Implements Copter::Mode.
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overridevirtual |
Implements Copter::Mode.
Definition at line 219 of file mode_flowhold.cpp.
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Definition at line 376 of file mode_flowhold.cpp.
Referenced by run().
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Definition at line 714 of file Copter.h.
Referenced by flowhold_flow_to_angle().
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Definition at line 735 of file Copter.h.
Referenced by flowhold_flow_to_angle().
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Definition at line 723 of file Copter.h.
Referenced by update_height_estimate().
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Definition at line 697 of file Copter.h.
Referenced by flowhold_flow_to_angle(), init(), and run().
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Definition at line 710 of file Copter.h.
Referenced by flowhold_flow_to_angle().
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Definition at line 711 of file Copter.h.
Referenced by flowhold_flow_to_angle(), init(), and run().
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Definition at line 708 of file Copter.h.
Referenced by flowhold_flow_to_angle().
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Definition at line 705 of file Copter.h.
Referenced by flowhold_flow_to_angle(), and update_height_estimate().
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Definition at line 732 of file Copter.h.
Referenced by flowhold_flow_to_angle(), init(), and update_height_estimate().
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Definition at line 729 of file Copter.h.
Referenced by update_height_estimate().
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Definition at line 726 of file Copter.h.
Referenced by update_height_estimate().
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Definition at line 731 of file Copter.h.
Referenced by init(), and update_height_estimate().
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Definition at line 738 of file Copter.h.
Referenced by flowhold_flow_to_angle().
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Definition at line 719 of file Copter.h.
Referenced by flowhold_flow_to_angle(), and init().
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Definition at line 718 of file Copter.h.
Referenced by flowhold_flow_to_angle().
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Definition at line 716 of file Copter.h.
Referenced by flowhold_flow_to_angle(), init(), and run().
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static |
Definition at line 678 of file Copter.h.
Referenced by ModeFlowHold().
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private |
Definition at line 720 of file Copter.h.
Referenced by flowhold_flow_to_angle().
1.8.13