/// @file AP_MotorsCoax.h /// @brief Motor and Servo control class for Co-axial helicopters with two motors and two flaps #pragma once #include #include // ArduPilot Mega Vector/Matrix math Library #include #include "AP_MotorsMulticopter.h" // feedback direction #define AP_MOTORS_COAX_POSITIVE 1 #define AP_MOTORS_COAX_NEGATIVE -1 #define NUM_ACTUATORS 4 #define AP_MOTORS_SINGLE_SPEED_DIGITAL_SERVOS 250 // update rate for digital servos #define AP_MOTORS_SINGLE_SPEED_ANALOG_SERVOS 125 // update rate for analog servos #define AP_MOTORS_COAX_SERVO_INPUT_RANGE 4500 // roll or pitch input of -4500 will cause servos to their minimum (i.e. radio_min), +4500 will move them to their maximum (i.e. radio_max) /// @class AP_MotorsSingle class AP_MotorsCoax : public AP_MotorsMulticopter { public: /// Constructor AP_MotorsCoax(uint16_t loop_rate, uint16_t speed_hz = AP_MOTORS_SPEED_DEFAULT) : AP_MotorsMulticopter(loop_rate, speed_hz) { }; // init void init(motor_frame_class frame_class, motor_frame_type frame_type) override; // set frame class (i.e. quad, hexa, heli) and type (i.e. x, plus) void set_frame_class_and_type(motor_frame_class frame_class, motor_frame_type frame_type) override; // set update rate to motors - a value in hertz void set_update_rate( uint16_t speed_hz ) override; // output_test_seq - spin a motor at the pwm value specified // motor_seq is the motor's sequence number from 1 to the number of motors on the frame // pwm value is an actual pwm value that will be output, normally in the range of 1000 ~ 2000 virtual void output_test_seq(uint8_t motor_seq, int16_t pwm) override; // output_to_motors - sends minimum values out to the motors virtual void output_to_motors() override; // get_motor_mask - returns a bitmask of which outputs are being used for motors or servos (1 means being used) // this can be used to ensure other pwm outputs (i.e. for servos) do not conflict uint16_t get_motor_mask() override; protected: // output - sends commands to the motors void output_armed_stabilizing() override; float _actuator_out[NUM_ACTUATORS]; // combined roll, pitch, yaw and throttle outputs to motors in 0~1 range float _thrust_yt_ccw; float _thrust_yt_cw; };