SITL: added SingleCopter simulator

This commit is contained in:
Andrew Tridgell 2016-05-26 16:29:06 +10:00
parent f9fb098222
commit 8944d298ed
2 changed files with 147 additions and 0 deletions

View File

@ -0,0 +1,94 @@
/// -*- 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/>.
*/
/*
singlecopter simulator class
*/
#include "SIM_SingleCopter.h"
#include <stdio.h>
using namespace SITL;
SingleCopter::SingleCopter(const char *home_str, const char *frame_str) :
Aircraft(home_str, frame_str)
{
mass = 2.0f;
/*
scaling from motor power to Newtons. Allows the copter
to hover against gravity when the motor is at hover_throttle
*/
thrust_scale = (mass * GRAVITY_MSS) / hover_throttle;
frame_height = 0.1;
}
/*
update the copter simulation by one time step
*/
void SingleCopter::update(const struct sitl_input &input)
{
// get wind vector setup
update_wind(input);
float actuator[4];
for (uint8_t i=0; i<4; i++) {
actuator[i] = constrain_float((input.servos[i]-1500) / 500.0f, -1, 1);
}
float thrust = constrain_float((input.servos[4]-1000) / 1000.0f, 0, 1);
float yaw_thrust = (actuator[0] + actuator[1] + actuator[2] + actuator[3]) * 0.25f * thrust;
float roll_thrust = (actuator[0] - actuator[2]) * 0.5f * thrust;
float pitch_thrust = (actuator[1] - actuator[3]) * 0.5f * thrust;
float torque_effect_accel = thrust * rotor_rot_accel;
// rotational acceleration, in rad/s/s, in body frame
Vector3f rot_accel(roll_thrust * roll_rate_max,
pitch_thrust * pitch_rate_max,
yaw_thrust * yaw_rate_max + torque_effect_accel);
// rotational air resistance
rot_accel.x -= gyro.x * radians(5000.0) / terminal_rotation_rate;
rot_accel.y -= gyro.y * radians(5000.0) / terminal_rotation_rate;
rot_accel.z -= gyro.z * radians(400.0) / terminal_rotation_rate;
// air resistance
Vector3f air_resistance = -velocity_air_ef * (GRAVITY_MSS/terminal_velocity);
// scale thrust to newtons
thrust *= thrust_scale;
accel_body = Vector3f(0, 0, -thrust / mass);
accel_body += dcm * air_resistance;
bool was_on_ground = on_ground(position);
update_dynamics(rot_accel);
// constrain height to the ground
if (on_ground(position) && !was_on_ground) {
// zero roll/pitch, but keep yaw
float r, p, y;
dcm.to_euler(&r, &p, &y);
dcm.from_euler(0, 0, y);
position.z = -(ground_level + frame_height - home.alt*0.01f);
velocity_ef.zero();
}
// update lat/lon/altitude
update_position();
}

View File

@ -0,0 +1,53 @@
/// -*- 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/>.
*/
/*
single copter simulator class
*/
#pragma once
#include "SIM_Aircraft.h"
#include <AP_Motors/AP_Motors.h>
namespace SITL {
/*
a single copter simulator
*/
class SingleCopter : public Aircraft {
public:
SingleCopter(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 SingleCopter(home_str, frame_str);
}
private:
float terminal_rotation_rate = 4*radians(360.0f);
float hover_throttle = 0.65f;
float terminal_velocity = 40;
float rotor_rot_accel = radians(20) * AP_MOTORS_MATRIX_YAW_FACTOR_CW;
float roll_rate_max = radians(700);
float pitch_rate_max = radians(700);
float yaw_rate_max = radians(700);
float thrust_scale;
};
} // namespace SITL