/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
/*
   This program is free software: you can redistribute it and/or modify
   it under the terms of the GNU General Public License as published by
   the Free Software Foundation, either version 3 of the License, or
   (at your option) any later version.

   This program is distributed in the hope that it will be useful,
   but WITHOUT ANY WARRANTY; without even the implied warranty of
   MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
   GNU General Public License for more details.

   You should have received a copy of the GNU General Public License
   along with this program.  If not, see <http://www.gnu.org/licenses/>.
 */
/*
  simple electric motor simulation class
*/

#pragma once

#include "SIM_Aircraft.h"

namespace SITL {

/*
  class to describe a motor position
 */
class Motor {
public:
    float angle;
    float yaw_factor;
    uint8_t servo;
    uint8_t display_order;

    // support for tilting motors
    int8_t roll_servo = -1;
    float roll_min, roll_max;
    int8_t pitch_servo = -1;
    float pitch_min, pitch_max;

    Motor(uint8_t _servo, float _angle, float _yaw_factor, uint8_t _display_order) :
        servo(_servo), // what servo output drives this motor
        angle(_angle), // angle in degrees from front
        yaw_factor(_yaw_factor), // positive is clockwise
        display_order(_display_order) // order for clockwise display
    {}

    /*
      alternative constructor for tiltable motors
     */
    Motor(uint8_t _servo, float _angle, float _yaw_factor, uint8_t _display_order,
          int8_t _roll_servo, float _roll_min, float _roll_max,
          int8_t _pitch_servo, float _pitch_min, float _pitch_max) :
        servo(_servo), // what servo output drives this motor
        angle(_angle), // angle in degrees from front
        yaw_factor(_yaw_factor), // positive is clockwise
        display_order(_display_order), // order for clockwise display
        roll_servo(_roll_servo),
        roll_min(_roll_min),
        roll_max(_roll_max),
        pitch_servo(_pitch_servo),
        pitch_min(_pitch_min),
        pitch_max(_pitch_max)
    {}
    
    void calculate_forces(const Aircraft::sitl_input &input,
                          float thrust_scale,
                          uint8_t motor_offset,
                          Vector3f &rot_accel, // rad/sec
                          Vector3f &body_thrust) const; // Z is down
};
}