// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- /// @file AP_MotorsMatrix.h /// @brief Motor control class for Matrixcopters #ifndef __AP_MOTORS_MATRIX_H__ #define __AP_MOTORS_MATRIX_H__ #include #include // ArduPilot Mega Vector/Matrix math Library #include // RC Channel Library #include "AP_Motors_Class.h" #define AP_MOTORS_MATRIX_YAW_FACTOR_CW -1 #define AP_MOTORS_MATRIX_YAW_FACTOR_CCW 1 #define AP_MOTORS_MATRIX_YAW_LOWER_LIMIT_PWM 200 /// @class AP_MotorsMatrix class AP_MotorsMatrix : public AP_Motors { public: /// Constructor AP_MotorsMatrix( RC_Channel& rc_roll, RC_Channel& rc_pitch, RC_Channel& rc_throttle, RC_Channel& rc_yaw, uint16_t speed_hz = AP_MOTORS_SPEED_DEFAULT) : AP_Motors(rc_roll, rc_pitch, rc_throttle, rc_yaw, speed_hz) {}; // init virtual void Init(); // set update rate to motors - a value in hertz // you must have setup_motors before calling this virtual void set_update_rate( uint16_t speed_hz ); // set frame orientation (normally + or X) virtual void set_frame_orientation( uint8_t new_orientation ); // enable - starts allowing signals to be sent to motors virtual void enable(); // output_test - 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(uint8_t motor_seq, int16_t pwm); // output_min - sends minimum values out to the motors virtual void output_min(); // add_motor using just position and yaw_factor (or prop direction) void add_motor(int8_t motor_num, float angle_degrees, float yaw_factor, uint8_t testing_order); // remove_motor void remove_motor(int8_t motor_num); // remove_all_motors - removes all motor definitions void remove_all_motors(); // setup_motors - configures the motors for a given frame type - should be overwritten by child classes virtual void setup_motors() { remove_all_motors(); }; protected: // output - sends commands to the motors virtual void output_armed(); virtual void output_disarmed(); // add_motor using raw roll, pitch, throttle and yaw factors void add_motor_raw(int8_t motor_num, float roll_fac, float pitch_fac, float yaw_fac, uint8_t testing_order); float _roll_factor[AP_MOTORS_MAX_NUM_MOTORS]; // each motors contribution to roll float _pitch_factor[AP_MOTORS_MAX_NUM_MOTORS]; // each motors contribution to pitch float _yaw_factor[AP_MOTORS_MAX_NUM_MOTORS]; // each motors contribution to yaw (normally 1 or -1) uint8_t _test_order[AP_MOTORS_MAX_NUM_MOTORS]; // order of the motors in the test sequence }; #endif // AP_MOTORSMATRIX