// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: t -*- /// @file AP_MotorsHeli.h /// @brief Motor control class for Traditional Heli #ifndef AP_MOTORSHELI #define AP_MOTORSHELI #include #include #include #include // ArduPilot Mega Vector/Matrix math Library #include // RC Channel Library #include // ArduPilot Mega RC Library #include // below is required to make "map" function available to this library #if defined(ARDUINO) && ARDUINO >= 100 #include "Arduino.h" #else #include "WProgram.h" #endif #define AP_MOTORS_HELI_SPEED_DEFAULT 125 // default servo update rate for helicopters #define AP_MOTORS_HELI_SPEED_DIGITAL_SERVOS 125 // update rate for digital servos #define AP_MOTORS_HELI_SPEED_ANALOG_SERVOS 125 // update rate for analog servos #define AP_MOTORS_HELI_NUM_SWASHPLATE_SERVOS 3 // tail servo uses channel 7 #define AP_MOTORS_HELI_EXT_GYRO CH_7 // frame definitions #define AP_MOTORS_HELI_SWASH_CCPM 0 #define AP_MOTORS_HELI_SWASH_H1 1 // ext RSC definitions #define AP_MOTORS_HELI_EXT_RSC CH_8 #define AP_MOTORSHELI_RSC_MODE_CH8_PASSTHROUGH 1 #define AP_MOTORSHELI_RSC_MODE_EXT_GOV 2 class AP_HeliControls; /// @class AP_MotorsHeli class AP_MotorsHeli : public AP_Motors { public: /// Constructor AP_MotorsHeli( uint8_t APM_version, APM_RC_Class* rc_out, RC_Channel* rc_roll, RC_Channel* rc_pitch, RC_Channel* rc_throttle, RC_Channel* rc_yaw, RC_Channel* rc_8, RC_Channel* swash_servo_1, RC_Channel* swash_servo_2, RC_Channel* swash_servo_3, RC_Channel* yaw_servo, uint16_t speed_hz = AP_MOTORS_HELI_SPEED_DEFAULT) : AP_Motors(APM_version, rc_out, rc_roll, rc_pitch, rc_throttle, rc_yaw, speed_hz), _servo_1(swash_servo_1), _servo_2(swash_servo_2), _servo_3(swash_servo_3), _servo_4(yaw_servo), _rc_8(rc_8) { throttle_mid = 0; _roll_scaler = 1; _pitch_scaler = 1; _collective_scalar = 1; _swash_initialised = false; }; RC_Channel *_servo_1; RC_Channel *_servo_2; RC_Channel *_servo_3; RC_Channel *_servo_4; RC_Channel *_rc_8; AP_Int8 swash_type; AP_Int16 servo1_pos; AP_Int16 servo2_pos; AP_Int16 servo3_pos; AP_Int16 collective_min; AP_Int16 collective_max; AP_Int16 collective_mid; AP_Int16 ext_gyro_enabled; AP_Int16 ext_gyro_gain; AP_Int16 roll_max; AP_Int16 pitch_max; AP_Int16 phase_angle; AP_Int16 collective_yaw_effect; AP_Int8 servo_manual; // used to trigger swash reset from mission planner AP_Int16 ext_gov_setpoint; // maximum output to the motor governor AP_Int8 rsc_mode; // sets the mode for rotor speed controller AP_Int16 rsc_ramp_up_rate; // sets the time in 100th seconds the RSC takes to ramp up to speed AP_Int8 acro_mode; // selects FBL Acro Mode, or Flybarred Acro Mode int16_t throttle_mid; // throttle mid point in pwm form (i.e. 0 ~ 1000) // init void Init(); // set update rate to motors - a value in hertz or AP_MOTORS_SPEED_INSTANT_PWM for instant pwm // you must have setup_motors before calling this void set_update_rate( uint16_t speed_hz ); // enable - starts allowing signals to be sent to motors void enable(); // get basic information about the platform uint8_t get_num_motors() { return 5; }; // motor test void output_test(); // output_min - sends minimum values out to the motors void output_min(); // init_swash - initialise the swash plate void init_swash(); // output - sends commands to the motors void output_armed(); // var_info for holding Parameter information static const struct AP_Param::GroupInfo var_info[]; protected: // heli_move_swash - moves swash plate to attitude of parameters passed in void move_swash(int16_t roll_out, int16_t pitch_out, int16_t coll_out, int16_t yaw_out); // reset_swash - free up swash for maximum movements. Used for set-up void reset_swash(); void output_disarmed(); void rsc_control(); float _rollFactor[AP_MOTORS_HELI_NUM_SWASHPLATE_SERVOS]; float _pitchFactor[AP_MOTORS_HELI_NUM_SWASHPLATE_SERVOS]; float _collectiveFactor[AP_MOTORS_HELI_NUM_SWASHPLATE_SERVOS]; // internally used variables float _roll_scaler; // scaler to convert roll input from radio (i.e. -4500 ~ 4500) to max roll range float _pitch_scaler; // scaler to convert pitch input from radio (i.e. -4500 ~ 4500) to max pitch range float _collective_scalar; // throttle scalar to convert pwm form (i.e. 0 ~ 1000) passed in to actual servo range (i.e 1250~1750 would be 500) bool _swash_initialised; // true if swash has been initialised int16_t rsc_output; // final output to the external motor governor 1000-2000 int16_t rsc_ramp; // current state of ramping }; #endif // AP_MOTORSHELI