/// -*- 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 . */ /* multicopter simulator 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; 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 {} }; /* class to describe a multicopter frame type */ class Frame { public: const char *name; uint8_t num_motors; const Motor *motors; Frame(const char *_name, uint8_t _num_motors, const Motor *_motors) : name(_name), num_motors(_num_motors), motors(_motors) {} // find a frame by name static Frame *find_frame(const char *name); // initialise frame void init(float mass, float hover_throttle, float terminal_velocity, float terminal_rotation_rate); // calculate rotational and linear accelerations void calculate_forces(const Aircraft &aircraft, const Aircraft::sitl_input &input, Vector3f &rot_accel, Vector3f &body_accel); float terminal_velocity; float terminal_rotation_rate; float thrust_scale; float mass; uint8_t motor_offset; }; /* a multicopter simulator */ class MultiCopter : public Aircraft { public: MultiCopter(const char *home_str, const char *frame_str); /* update model by one time step */ void update(const struct sitl_input &input); /* static object creator */ static Aircraft *create(const char *home_str, const char *frame_str) { return new MultiCopter(home_str, frame_str); } protected: // calculate rotational and linear accelerations void calculate_forces(const struct sitl_input &input, Vector3f &rot_accel, Vector3f &body_accel); Frame *frame; }; } // namespace SITL