mirror of https://github.com/ArduPilot/ardupilot
53 lines
1.2 KiB
C
53 lines
1.2 KiB
C
#pragma once
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#include <AP_Param/AP_Param.h>
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/*
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common parameters for fixed wing aircraft
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*/
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struct AP_FixedWing {
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AP_Int8 throttle_min;
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AP_Int8 throttle_max;
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AP_Int8 throttle_slewrate;
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AP_Int8 throttle_cruise;
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AP_Int8 takeoff_throttle_max;
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AP_Int16 airspeed_min;
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AP_Int16 airspeed_max;
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AP_Float airspeed_cruise;
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AP_Float airspeed_stall;
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AP_Float min_groundspeed;
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AP_Int8 crash_detection_enable;
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AP_Float roll_limit;
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AP_Float pitch_limit_max;
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AP_Float pitch_limit_min;
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AP_Int8 autotune_level;
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AP_Int32 autotune_options;
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AP_Int8 stall_prevention;
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AP_Int16 loiter_radius;
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AP_Float takeoff_throttle_max_t;
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struct Rangefinder_State {
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bool in_range:1;
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bool have_initial_reading:1;
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bool in_use:1;
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float initial_range;
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float correction;
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float initial_correction;
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float last_stable_correction;
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uint32_t last_correction_time_ms;
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uint8_t in_range_count;
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float height_estimate;
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float last_distance;
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};
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// stages of flight
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enum class FlightStage {
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TAKEOFF = 1,
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VTOL = 2,
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NORMAL = 3,
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LAND = 4,
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ABORT_LANDING = 7
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};
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};
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