2 changed files with 147 additions and 0 deletions
@ -0,0 +1,94 @@
@@ -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(); |
||||
} |
@ -0,0 +1,53 @@
@@ -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
|
Loading…
Reference in new issue