2014-02-06 08:28:55 -04:00
// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
2014-02-06 10:39:30 -04:00
/// @file AP_MotorsCoax.h
/// @brief Motor and Servo control class for Co-axial helicopters with two motors and two flaps
2016-02-17 21:25:38 -04:00
# pragma once
2014-02-06 08:28:55 -04:00
2015-08-11 03:28:44 -03:00
# include <AP_Common/AP_Common.h>
# include <AP_Math/AP_Math.h> // ArduPilot Mega Vector/Matrix math Library
# include <RC_Channel/RC_Channel.h> // RC Channel Library
2015-07-15 04:57:15 -03:00
# include "AP_MotorsMulticopter.h"
2014-02-06 08:28:55 -04:00
// feedback direction
# define AP_MOTORS_COAX_POSITIVE 1
# define AP_MOTORS_COAX_NEGATIVE -1
2016-01-19 23:56:58 -04:00
# define NUM_ACTUATORS 4
2014-02-06 08:28:55 -04:00
# 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
2014-02-06 10:39:30 -04:00
# 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)
2014-02-06 08:28:55 -04:00
/// @class AP_MotorsSingle
2015-07-15 04:57:15 -03:00
class AP_MotorsCoax : public AP_MotorsMulticopter {
2014-02-06 08:28:55 -04:00
public :
/// Constructor
2016-01-20 08:11:39 -04:00
AP_MotorsCoax ( uint16_t loop_rate , uint16_t speed_hz = AP_MOTORS_SPEED_DEFAULT ) :
2015-07-15 04:57:15 -03:00
AP_MotorsMulticopter ( loop_rate , speed_hz ) ,
2016-01-20 08:11:39 -04:00
_servo1 ( CH_1 ) , _servo2 ( CH_2 ) , _servo3 ( CH_3 ) , _servo4 ( CH_4 )
2014-02-06 08:28:55 -04:00
{
AP_Param : : setup_object_defaults ( this , var_info ) ;
} ;
// init
virtual void Init ( ) ;
// set update rate to motors - a value in hertz
void set_update_rate ( uint16_t speed_hz ) ;
// enable - starts allowing signals to be sent to motors
virtual void enable ( ) ;
2014-04-28 04:29:30 -03:00
// 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 ) ;
2014-02-06 08:28:55 -04:00
2016-01-19 23:57:21 -04:00
// output_to_motors - sends minimum values out to the motors
virtual void output_to_motors ( ) ;
2014-07-26 04:29:31 -03:00
// 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
2016-01-19 23:54:01 -04:00
virtual uint16_t get_motor_mask ( ) ;
2014-07-26 04:29:31 -03:00
2014-02-06 08:28:55 -04:00
// var_info for holding Parameter information
static const struct AP_Param : : GroupInfo var_info [ ] ;
protected :
// output - sends commands to the motors
2015-04-02 17:54:15 -03:00
void output_armed_stabilizing ( ) ;
2014-02-06 08:28:55 -04:00
2016-01-21 21:19:13 -04:00
// servo speed
AP_Int16 _servo_speed ;
2016-01-20 08:11:39 -04:00
2016-01-19 23:54:01 -04:00
// Allow the use of a 4 servo output to make it easy to test coax and single using same airframe
2016-01-20 08:11:39 -04:00
RC_Channel _servo1 ;
RC_Channel _servo2 ;
RC_Channel _servo3 ;
RC_Channel _servo4 ;
2016-01-19 23:54:01 -04:00
2016-01-19 23:56:58 -04:00
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 ;
2014-02-06 08:28:55 -04:00
} ;