mirror of
https://github.com/ArduPilot/ardupilot
synced 2025-01-03 06:28:27 -04:00
SITL: Add support for Sub
This commit is contained in:
parent
aec7091faa
commit
36f3cae535
50
libraries/SITL/Frame_Vectored.h
Normal file
50
libraries/SITL/Frame_Vectored.h
Normal file
@ -0,0 +1,50 @@
|
|||||||
|
#pragma once
|
||||||
|
|
||||||
|
using namespace SITL;
|
||||||
|
|
||||||
|
#define MOT_1_ROLL_FACTOR 0.0
|
||||||
|
#define MOT_1_PITCH_FACTOR 0.0
|
||||||
|
#define MOT_1_YAW_FACTOR 1.0
|
||||||
|
#define MOT_1_THROTTLE_FACTOR 0.0
|
||||||
|
#define MOT_1_FORWARD_FACTOR -1
|
||||||
|
#define MOT_1_STRAFE_FACTOR 1
|
||||||
|
|
||||||
|
//Front left
|
||||||
|
#define MOT_2_ROLL_FACTOR 0.0
|
||||||
|
#define MOT_2_PITCH_FACTOR 0.0
|
||||||
|
#define MOT_2_YAW_FACTOR -1.0
|
||||||
|
#define MOT_2_THROTTLE_FACTOR 0.0
|
||||||
|
#define MOT_2_FORWARD_FACTOR -1
|
||||||
|
#define MOT_2_STRAFE_FACTOR -1
|
||||||
|
|
||||||
|
//Back right
|
||||||
|
#define MOT_3_ROLL_FACTOR 0
|
||||||
|
#define MOT_3_PITCH_FACTOR 0
|
||||||
|
#define MOT_3_YAW_FACTOR -1.0
|
||||||
|
#define MOT_3_THROTTLE_FACTOR 0.0
|
||||||
|
#define MOT_3_FORWARD_FACTOR 1
|
||||||
|
#define MOT_3_STRAFE_FACTOR 1
|
||||||
|
|
||||||
|
//Back left
|
||||||
|
#define MOT_4_ROLL_FACTOR 0
|
||||||
|
#define MOT_4_PITCH_FACTOR 0
|
||||||
|
#define MOT_4_YAW_FACTOR 1.0
|
||||||
|
#define MOT_4_THROTTLE_FACTOR 0.0
|
||||||
|
#define MOT_4_FORWARD_FACTOR 1
|
||||||
|
#define MOT_4_STRAFE_FACTOR -1
|
||||||
|
|
||||||
|
//Right facing up
|
||||||
|
#define MOT_5_ROLL_FACTOR 1.0
|
||||||
|
#define MOT_5_PITCH_FACTOR 0.0
|
||||||
|
#define MOT_5_YAW_FACTOR 0.0
|
||||||
|
#define MOT_5_THROTTLE_FACTOR -1
|
||||||
|
#define MOT_5_FORWARD_FACTOR 0.0
|
||||||
|
#define MOT_5_STRAFE_FACTOR 0.0
|
||||||
|
|
||||||
|
//Left facing up
|
||||||
|
#define MOT_6_ROLL_FACTOR -1.0
|
||||||
|
#define MOT_6_PITCH_FACTOR 0.0
|
||||||
|
#define MOT_6_YAW_FACTOR 0.0
|
||||||
|
#define MOT_6_THROTTLE_FACTOR -1
|
||||||
|
#define MOT_6_FORWARD_FACTOR 0.0
|
||||||
|
#define MOT_6_STRAFE_FACTOR 0.0
|
96
libraries/SITL/SIM_Submarine.cpp
Normal file
96
libraries/SITL/SIM_Submarine.cpp
Normal file
@ -0,0 +1,96 @@
|
|||||||
|
/*
|
||||||
|
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/>.
|
||||||
|
*/
|
||||||
|
/*
|
||||||
|
Submarine simulator class
|
||||||
|
*/
|
||||||
|
|
||||||
|
#include "SIM_Submarine.h"
|
||||||
|
#include <AP_Motors/AP_Motors.h>
|
||||||
|
#include "Frame_Vectored.h"
|
||||||
|
|
||||||
|
using namespace SITL;
|
||||||
|
|
||||||
|
static Thruster vectored_thrusters[] =
|
||||||
|
{
|
||||||
|
Thruster(0, MOT_1_ROLL_FACTOR, MOT_1_PITCH_FACTOR, MOT_1_YAW_FACTOR, MOT_1_THROTTLE_FACTOR, MOT_1_FORWARD_FACTOR, MOT_1_STRAFE_FACTOR),
|
||||||
|
Thruster(1, MOT_2_ROLL_FACTOR, MOT_2_PITCH_FACTOR, MOT_2_YAW_FACTOR, MOT_2_THROTTLE_FACTOR, MOT_2_FORWARD_FACTOR, MOT_2_STRAFE_FACTOR),
|
||||||
|
Thruster(2, MOT_3_ROLL_FACTOR, MOT_3_PITCH_FACTOR, MOT_3_YAW_FACTOR, MOT_3_THROTTLE_FACTOR, MOT_3_FORWARD_FACTOR, MOT_3_STRAFE_FACTOR),
|
||||||
|
Thruster(3, MOT_4_ROLL_FACTOR, MOT_4_PITCH_FACTOR, MOT_4_YAW_FACTOR, MOT_4_THROTTLE_FACTOR, MOT_4_FORWARD_FACTOR, MOT_4_STRAFE_FACTOR),
|
||||||
|
Thruster(4, MOT_5_ROLL_FACTOR, MOT_5_PITCH_FACTOR, MOT_5_YAW_FACTOR, MOT_5_THROTTLE_FACTOR, MOT_5_FORWARD_FACTOR, MOT_5_STRAFE_FACTOR),
|
||||||
|
Thruster(5, MOT_6_ROLL_FACTOR, MOT_6_PITCH_FACTOR, MOT_6_YAW_FACTOR, MOT_6_THROTTLE_FACTOR, MOT_6_FORWARD_FACTOR, MOT_6_STRAFE_FACTOR)
|
||||||
|
|
||||||
|
};
|
||||||
|
|
||||||
|
Submarine::Submarine(const char *home_str, const char *frame_str) :
|
||||||
|
Aircraft(home_str, frame_str),
|
||||||
|
frame(NULL)
|
||||||
|
{
|
||||||
|
frame_height = 0.1;
|
||||||
|
ground_behavior = GROUND_BEHAVIOR_NONE;
|
||||||
|
}
|
||||||
|
|
||||||
|
// calculate rotational and linear accelerations
|
||||||
|
void Submarine::calculate_forces(const struct sitl_input &input, Vector3f &rot_accel, Vector3f &body_accel)
|
||||||
|
{
|
||||||
|
rot_accel = Vector3f(0,0,0);
|
||||||
|
body_accel = Vector3f(0,0,0);
|
||||||
|
for (int i = 0; i < 6; i++) {
|
||||||
|
Thruster t = vectored_thrusters[i];
|
||||||
|
int16_t pwm = input.servos[t.servo];
|
||||||
|
float output = 0;
|
||||||
|
if (pwm < 2000 && pwm > 1000) {
|
||||||
|
output = (pwm - 1500) / 400.0f; // range -1~1
|
||||||
|
}
|
||||||
|
|
||||||
|
body_accel += t.linear * output * 1.2 * GRAVITY_MSS;
|
||||||
|
rot_accel += t.rotational * output;
|
||||||
|
}
|
||||||
|
|
||||||
|
float terminal_rotation_rate = 10.0;
|
||||||
|
if (terminal_rotation_rate > 0) {
|
||||||
|
// rotational air resistance
|
||||||
|
rot_accel.x -= gyro.x * radians(400.0) / terminal_rotation_rate;
|
||||||
|
rot_accel.y -= gyro.y * radians(400.0) / terminal_rotation_rate;
|
||||||
|
rot_accel.z -= gyro.z * radians(400.0) / terminal_rotation_rate;
|
||||||
|
}
|
||||||
|
|
||||||
|
float terminal_velocity = 3.0;
|
||||||
|
if (terminal_velocity > 0) {
|
||||||
|
// air resistance
|
||||||
|
Vector3f air_resistance = -velocity_air_ef * (GRAVITY_MSS/terminal_velocity);
|
||||||
|
body_accel += dcm.transposed() * air_resistance;
|
||||||
|
}
|
||||||
|
}
|
||||||
|
|
||||||
|
/*
|
||||||
|
update the Submarine simulation by one time step
|
||||||
|
*/
|
||||||
|
void Submarine::update(const struct sitl_input &input)
|
||||||
|
{
|
||||||
|
// get wind vector setup
|
||||||
|
update_wind(input);
|
||||||
|
|
||||||
|
Vector3f rot_accel;
|
||||||
|
|
||||||
|
calculate_forces(input, rot_accel, accel_body);
|
||||||
|
|
||||||
|
update_dynamics(rot_accel);
|
||||||
|
|
||||||
|
// update lat/lon/altitude
|
||||||
|
update_position();
|
||||||
|
|
||||||
|
// update magnetic field
|
||||||
|
update_mag_field_bf();
|
||||||
|
}
|
62
libraries/SITL/SIM_Submarine.h
Normal file
62
libraries/SITL/SIM_Submarine.h
Normal file
@ -0,0 +1,62 @@
|
|||||||
|
/*
|
||||||
|
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/>.
|
||||||
|
*/
|
||||||
|
/*
|
||||||
|
ROV/AUV/Submarine simulator class
|
||||||
|
*/
|
||||||
|
|
||||||
|
#pragma once
|
||||||
|
|
||||||
|
#include "SIM_Aircraft.h"
|
||||||
|
#include "SIM_Motor.h"
|
||||||
|
#include "SIM_Frame.h"
|
||||||
|
|
||||||
|
namespace SITL {
|
||||||
|
|
||||||
|
/*
|
||||||
|
a submarine simulator
|
||||||
|
*/
|
||||||
|
|
||||||
|
|
||||||
|
class Submarine : public Aircraft {
|
||||||
|
public:
|
||||||
|
Submarine(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 Submarine(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;
|
||||||
|
};
|
||||||
|
|
||||||
|
class Thruster {
|
||||||
|
public:
|
||||||
|
Thruster(int8_t _servo, float roll_fac, float pitch_fac, float yaw_fac, float throttle_fac, float forward_fac, float lat_fac) :
|
||||||
|
servo(_servo)
|
||||||
|
{
|
||||||
|
linear = Vector3f(forward_fac, lat_fac, -throttle_fac);
|
||||||
|
rotational = Vector3f(roll_fac, pitch_fac, yaw_fac);
|
||||||
|
};
|
||||||
|
int8_t servo;
|
||||||
|
Vector3f linear;
|
||||||
|
Vector3f rotational;
|
||||||
|
};
|
||||||
|
}
|
Loading…
Reference in New Issue
Block a user