ardupilot/libraries/SITL/SIM_SilentWings.h

113 lines
4.5 KiB
C
Raw Permalink Normal View History

/*
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/>.
*/
#pragma once
#include <AP_HAL/utility/Socket.h>
#include "SIM_Aircraft.h"
namespace SITL {
/*
A wrapper for a simulated Silent Wings aircraft.
*/
class SilentWings : public Aircraft {
public:
2019-08-15 01:01:24 -03:00
SilentWings(const char *frame_str);
/* Updates the aircraft model by one time step */
void update(const struct sitl_input &input) override;
/* Static object creator */
2019-08-15 01:01:24 -03:00
static Aircraft *create(const char *frame_str) {
return new SilentWings(frame_str);
}
private:
/* Reply packet sent from SilentWings to ArduPlane */
struct PACKED fdm_packet {
unsigned int timestamp; // Millisec Timestamp
double position_latitude; // Degrees Position latitude,
double position_longitude; // Degrees longitude,
float altitude_msl; // m Altitude w.r.t. the sea level
float altitude_ground; // m Altitude w.r.t. the ground level
float altitude_ground_45; // m Ground 45 degrees ahead (NOT IMPLEMENTED YET)
float altitude_ground_forward; // m Ground straight ahead (NOT IMPLEMENTED YET)
float roll; // Degrees
float pitch; // Degrees
float yaw; // Degrees
float d_roll; // Deg/sec Roll speed
float d_pitch; // Deg/sec Pitch speed
float d_yaw; // Deg/sec Yaw speed
float vx; // m/s Velocity vector in body-axis
float vy;
float vz;
float vx_wind; // m/s Velocity vector in body-axis, relative to the wind
float vy_wind;
float vz_wind;
float v_eas; // m/s Equivalent (indicated) air speed.
float ax; // m/s^2 Acceleration vector in body axis
float ay;
float az;
float angle_of_attack; // Degrees Angle of attack
float angle_sideslip; // Degrees Sideslip angle
float vario; // m/s Total energy-compensated variometer
float heading; // Degrees Compass heading
float rate_of_turn; // Deg/sec Rate of turn
float airpressure; // Pa Local air pressure at aircraft altitude)
float density; // Air density at aircraft altitude
float temperature; // Degrees Celcius Air temperature at aircraft altitude
} pkt;
struct {
uint32_t last_report_ms;
uint32_t data_count;
uint32_t frame_count;
} report;
bool recv_fdm(void);
void process_packet();
bool interim_update();
/* Create and set in/out socket for Silent Wings simulator */
void set_interface_ports(const char* address, const int port_in, const int port_out) override;
/* Sends control inputs to the Silent Wings. */
void send_servos(const struct sitl_input &input);
/* Timestamp of the latest data packet received from Silent Wings. */
uint32_t last_data_time_ms;
/* Timestamp of the first data packet received from Silent Wings. */
uint32_t first_pkt_timestamp_ms;
/* Indicates whether first_pkt_timestamp_ms has been initialized (i.e., any packets have been received from Silent Wings. */
bool inited_first_pkt_timestamp;
/* ArduPlane's internal time when the first packet from Silent Wings is received. */
uint64_t time_base_us;
SocketAPM sock;
const char *_sw_address = "127.0.0.1";
int _port_in = 6060;
int _sw_port = 6070;
bool home_initialized;
};
} // namespace SITL