mirror of https://github.com/ArduPilot/ardupilot
SITL: added SingleCopter simulator
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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singlecopter simulator class
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*/
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#include "SIM_SingleCopter.h"
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#include <stdio.h>
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using namespace SITL;
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SingleCopter::SingleCopter(const char *home_str, const char *frame_str) :
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Aircraft(home_str, frame_str)
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{
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mass = 2.0f;
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/*
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scaling from motor power to Newtons. Allows the copter
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to hover against gravity when the motor is at hover_throttle
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*/
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thrust_scale = (mass * GRAVITY_MSS) / hover_throttle;
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frame_height = 0.1;
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}
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/*
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update the copter simulation by one time step
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*/
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void SingleCopter::update(const struct sitl_input &input)
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{
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// get wind vector setup
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update_wind(input);
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float actuator[4];
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for (uint8_t i=0; i<4; i++) {
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actuator[i] = constrain_float((input.servos[i]-1500) / 500.0f, -1, 1);
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}
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float thrust = constrain_float((input.servos[4]-1000) / 1000.0f, 0, 1);
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float yaw_thrust = (actuator[0] + actuator[1] + actuator[2] + actuator[3]) * 0.25f * thrust;
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float roll_thrust = (actuator[0] - actuator[2]) * 0.5f * thrust;
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float pitch_thrust = (actuator[1] - actuator[3]) * 0.5f * thrust;
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float torque_effect_accel = thrust * rotor_rot_accel;
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// rotational acceleration, in rad/s/s, in body frame
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Vector3f rot_accel(roll_thrust * roll_rate_max,
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pitch_thrust * pitch_rate_max,
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yaw_thrust * yaw_rate_max + torque_effect_accel);
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// rotational air resistance
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rot_accel.x -= gyro.x * radians(5000.0) / terminal_rotation_rate;
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rot_accel.y -= gyro.y * radians(5000.0) / terminal_rotation_rate;
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rot_accel.z -= gyro.z * radians(400.0) / terminal_rotation_rate;
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// air resistance
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Vector3f air_resistance = -velocity_air_ef * (GRAVITY_MSS/terminal_velocity);
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// scale thrust to newtons
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thrust *= thrust_scale;
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accel_body = Vector3f(0, 0, -thrust / mass);
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accel_body += dcm * air_resistance;
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bool was_on_ground = on_ground(position);
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update_dynamics(rot_accel);
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// constrain height to the ground
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if (on_ground(position) && !was_on_ground) {
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// zero roll/pitch, but keep yaw
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float r, p, y;
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dcm.to_euler(&r, &p, &y);
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dcm.from_euler(0, 0, y);
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position.z = -(ground_level + frame_height - home.alt*0.01f);
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velocity_ef.zero();
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}
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// update lat/lon/altitude
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update_position();
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}
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@ -0,0 +1,53 @@
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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single copter simulator class
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*/
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#pragma once
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#include "SIM_Aircraft.h"
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#include <AP_Motors/AP_Motors.h>
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namespace SITL {
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/*
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a single copter simulator
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*/
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class SingleCopter : public Aircraft {
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public:
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SingleCopter(const char *home_str, const char *frame_str);
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/* update model by one time step */
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void update(const struct sitl_input &input);
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/* static object creator */
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static Aircraft *create(const char *home_str, const char *frame_str) {
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return new SingleCopter(home_str, frame_str);
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}
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private:
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float terminal_rotation_rate = 4*radians(360.0f);
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float hover_throttle = 0.65f;
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float terminal_velocity = 40;
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float rotor_rot_accel = radians(20) * AP_MOTORS_MATRIX_YAW_FACTOR_CW;
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float roll_rate_max = radians(700);
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float pitch_rate_max = radians(700);
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float yaw_rate_max = radians(700);
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float thrust_scale;
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};
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} // namespace SITL
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