#pragma once #include "Blimp.h" class Parameters; class ParametersG2; class GCS_Blimp; class Mode { public: // Auto Pilot Modes enumeration enum class Number : uint8_t { MANUAL = 0, // manual control similar to Copter's stabilize mode LAND = 1, // currently just stops moving // STABILIZE = 0, // manual airframe angle with manual throttle // ACRO = 1, // manual body-frame angular rate with manual throttle // ALT_HOLD = 2, // manual airframe angle with automatic throttle // AUTO = 3, // fully automatic waypoint control using mission commands // GUIDED = 4, // fully automatic fly to coordinate or fly at velocity/direction using GCS immediate commands // LOITER = 5, // automatic horizontal acceleration with automatic throttle // RTL = 6, // automatic return to launching point // CIRCLE = 7, // automatic circular flight with automatic throttle // LAND = 9, // automatic landing with horizontal position control // DRIFT = 11, // semi-automous position, yaw and throttle control // SPORT = 13, // manual earth-frame angular rate control with manual throttle // FLIP = 14, // automatically flip the vehicle on the roll axis // AUTOTUNE = 15, // automatically tune the vehicle's roll and pitch gains // POSHOLD = 16, // automatic position hold with manual override, with automatic throttle // BRAKE = 17, // full-brake using inertial/GPS system, no pilot input // THROW = 18, // throw to launch mode using inertial/GPS system, no pilot input // AVOID_ADSB = 19, // automatic avoidance of obstacles in the macro scale - e.g. full-sized aircraft // GUIDED_NOGPS = 20, // guided mode but only accepts attitude and altitude // SMART_RTL = 21, // SMART_RTL returns to home by retracing its steps // FLOWHOLD = 22, // FLOWHOLD holds position with optical flow without rangefinder // FOLLOW = 23, // follow attempts to follow another vehicle or ground station // ZIGZAG = 24, // ZIGZAG mode is able to fly in a zigzag manner with predefined point A and point B // SYSTEMID = 25, // System ID mode produces automated system identification signals in the controllers // AUTOROTATE = 26, // Autonomous autorotation }; // constructor Mode(void); // do not allow copying Mode(const Mode &other) = delete; Mode &operator=(const Mode&) = delete; // child classes should override these methods virtual bool init(bool ignore_checks) { return true; } virtual void run() = 0; virtual bool requires_GPS() const = 0; virtual bool has_manual_throttle() const = 0; virtual bool allows_arming(bool from_gcs) const = 0; virtual bool is_autopilot() const { return false; } virtual bool has_user_takeoff(bool must_navigate) const { return false; } virtual bool in_guided_mode() const { return false; } virtual bool logs_attitude() const { return false; } // return a string for this flightmode virtual const char *name() const = 0; virtual const char *name4() const = 0; bool do_user_takeoff(float takeoff_alt_cm, bool must_navigate); // virtual bool is_taking_off() const; // static void takeoff_stop() { takeoff.stop(); } virtual bool is_landing() const { return false; } // mode requires terrain to be present to be functional virtual bool requires_terrain_failsafe() const { return false; } // functions for reporting to GCS virtual bool get_wp(Location &loc) { return false; }; virtual int32_t wp_bearing() const { return 0; } virtual uint32_t wp_distance() const { return 0; } virtual float crosstrack_error() const { return 0.0f; } void update_navigation(); int32_t get_alt_above_ground_cm(void); // pilot input processing void get_pilot_desired_accelerations(float &right_out, float &front_out) const; float get_pilot_desired_yaw_rate(int16_t stick_angle); float get_pilot_desired_throttle() const; // returns climb target_rate reduced to avoid obstacles and // altitude fence float get_avoidance_adjusted_climbrate(float target_rate); // const Vector3f& get_desired_velocity() { // // note that position control isn't used in every mode, so // // this may return bogus data: // return pos_control->get_desired_velocity(); // } protected: // navigation support functions virtual void run_autopilot() {} // helper functions bool is_disarmed_or_landed() const; void zero_throttle_and_relax_ac(bool spool_up = false); void zero_throttle_and_hold_attitude(); void make_safe_spool_down(); // functions to control landing // in modes that support landing void land_run_horizontal_control(); void land_run_vertical_control(bool pause_descent = false); // return expected input throttle setting to hover: virtual float throttle_hover() const; // convenience references to avoid code churn in conversion: Parameters &g; ParametersG2 &g2; AP_InertialNav &inertial_nav; AP_AHRS &ahrs; Fins *&motors; RC_Channel *&channel_right; RC_Channel *&channel_front; RC_Channel *&channel_down; RC_Channel *&channel_yaw; float &G_Dt; public: // Navigation Yaw control class AutoYaw { public: // yaw(): main product of AutoYaw; the heading: float yaw(); // mode(): current method of determining desired yaw: autopilot_yaw_mode mode() const { return (autopilot_yaw_mode)_mode; } void set_mode_to_default(bool rtl); void set_mode(autopilot_yaw_mode new_mode); autopilot_yaw_mode default_mode(bool rtl) const; // rate_cds(): desired yaw rate in centidegrees/second: float rate_cds() const; void set_rate(float new_rate_cds); // set_roi(...): set a "look at" location: void set_roi(const Location &roi_location); void set_fixed_yaw(float angle_deg, float turn_rate_dps, int8_t direction, bool relative_angle); private: float look_ahead_yaw(); float roi_yaw(); // auto flight mode's yaw mode uint8_t _mode = AUTO_YAW_LOOK_AT_NEXT_WP; // Yaw will point at this location if mode is set to AUTO_YAW_ROI Vector3f roi; // bearing from current location to the ROI float _roi_yaw; // yaw used for YAW_FIXED yaw_mode int32_t _fixed_yaw; // Deg/s we should turn int16_t _fixed_yaw_slewrate; // heading when in yaw_look_ahead_yaw float _look_ahead_yaw; // turn rate (in cds) when auto_yaw_mode is set to AUTO_YAW_RATE float _rate_cds; // used to reduce update rate to 100hz: uint8_t roi_yaw_counter; }; static AutoYaw auto_yaw; // pass-through functions to reduce code churn on conversion; // these are candidates for moving into the Mode base // class. float get_pilot_desired_climb_rate(float throttle_control); float get_non_takeoff_throttle(void); bool set_mode(Mode::Number mode, ModeReason reason); void set_land_complete(bool b); GCS_Blimp &gcs(); void set_throttle_takeoff(void); uint16_t get_pilot_speed_dn(void); // end pass-through functions }; class ModeManual : public Mode { public: // inherit constructor using Mode::Mode; virtual void run() override; bool requires_GPS() const override { return false; } bool has_manual_throttle() const override { return true; } bool allows_arming(bool from_gcs) const override { return true; }; bool is_autopilot() const override { return false; } protected: const char *name() const override { return "MANUAL"; } const char *name4() const override { return "MANU"; } private: }; class ModeLand : public Mode { public: // inherit constructor using Mode::Mode; virtual void run() override; bool requires_GPS() const override { return false; } bool has_manual_throttle() const override { return true; } bool allows_arming(bool from_gcs) const override { return false; }; bool is_autopilot() const override { return false; } protected: const char *name() const override { return "LAND"; } const char *name4() const override { return "LAND"; } private: };