ardupilot/libraries/SITL/SIM_FlightAxis.h

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/*
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/>.
*/
/*
simulator connection for ardupilot version of FlightAxis
*/
#pragma once
#include <AP_HAL/utility/Socket.h>
#include "SIM_Aircraft.h"
namespace SITL {
/*
a FlightAxis simulator
*/
class FlightAxis : public Aircraft {
public:
FlightAxis(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 FlightAxis(home_str, frame_str);
}
struct state {
double rcin[8];
double m_airspeed_MPS;
double m_altitudeASL_MTR;
double m_altitudeAGL_MTR;
double m_groundspeed_MPS;
double m_pitchRate_DEGpSEC;
double m_rollRate_DEGpSEC;
double m_yawRate_DEGpSEC;
double m_azimuth_DEG;
double m_inclination_DEG;
double m_roll_DEG;
double m_aircraftPositionX_MTR;
double m_aircraftPositionY_MTR;
double m_velocityWorldU_MPS;
double m_velocityWorldV_MPS;
double m_velocityWorldW_MPS;
double m_velocityBodyU_MPS;
double m_velocityBodyV_MPS;
double m_velocityBodyW_MPS;
double m_accelerationWorldAX_MPS2;
double m_accelerationWorldAY_MPS2;
double m_accelerationWorldAZ_MPS2;
double m_accelerationBodyAX_MPS2;
double m_accelerationBodyAY_MPS2;
double m_accelerationBodyAZ_MPS2;
double m_windX_MPS;
double m_windY_MPS;
double m_windZ_MPS;
double m_propRPM;
double m_heliMainRotorRPM;
double m_batteryVoltage_VOLTS;
double m_batteryCurrentDraw_AMPS;
double m_batteryRemainingCapacity_MAH;
double m_fuelRemaining_OZ;
double m_isLocked;
double m_hasLostComponents;
double m_anEngineIsRunning;
double m_isTouchingGround;
double m_currentAircraftStatus;
double m_currentPhysicsTime_SEC;
double m_currentPhysicsSpeedMultiplier;
double m_orientationQuaternion_X;
double m_orientationQuaternion_Y;
double m_orientationQuaternion_Z;
double m_orientationQuaternion_W;
double m_flightAxisControllerIsActive;
double m_resetButtonHasBeenPressed;
} state;
static const uint16_t num_keys = sizeof(state)/sizeof(double);
struct keytable {
const char *key;
double &ref;
} keytable[num_keys] = {
{ "item", state.rcin[0] },
{ "item", state.rcin[1] },
{ "item", state.rcin[2] },
{ "item", state.rcin[3] },
{ "item", state.rcin[4] },
{ "item", state.rcin[5] },
{ "item", state.rcin[6] },
{ "item", state.rcin[7] },
{ "m-airspeed-MPS", state.m_airspeed_MPS },
{ "m-altitudeASL-MTR", state.m_altitudeASL_MTR },
{ "m-altitudeAGL-MTR", state.m_altitudeAGL_MTR },
{ "m-groundspeed-MPS", state.m_groundspeed_MPS },
{ "m-pitchRate-DEGpSEC", state.m_pitchRate_DEGpSEC },
{ "m-rollRate-DEGpSEC", state.m_rollRate_DEGpSEC },
{ "m-yawRate-DEGpSEC", state.m_yawRate_DEGpSEC },
{ "m-azimuth-DEG", state.m_azimuth_DEG },
{ "m-inclination-DEG", state.m_inclination_DEG },
{ "m-roll-DEG", state.m_roll_DEG },
{ "m-aircraftPositionX-MTR", state.m_aircraftPositionX_MTR },
{ "m-aircraftPositionY-MTR", state.m_aircraftPositionY_MTR },
{ "m-velocityWorldU-MPS", state.m_velocityWorldU_MPS },
{ "m-velocityWorldV-MPS", state.m_velocityWorldV_MPS },
{ "m-velocityWorldW-MPS", state.m_velocityWorldW_MPS },
{ "m-velocityBodyU-MPS", state.m_velocityBodyU_MPS },
{ "m-velocityBodyV-MPS", state.m_velocityBodyV_MPS },
{ "m-velocityBodyW-MPS", state.m_velocityBodyW_MPS },
{ "m-accelerationWorldAX-MPS2", state.m_accelerationWorldAX_MPS2 },
{ "m-accelerationWorldAY-MPS2", state.m_accelerationWorldAY_MPS2 },
{ "m-accelerationWorldAZ-MPS2", state.m_accelerationWorldAZ_MPS2 },
{ "m-accelerationBodyAX-MPS2", state.m_accelerationBodyAX_MPS2 },
{ "m-accelerationBodyAY-MPS2", state.m_accelerationBodyAY_MPS2 },
{ "m-accelerationBodyAZ-MPS2", state.m_accelerationBodyAZ_MPS2 },
{ "m-windX-MPS", state.m_windX_MPS },
{ "m-windY-MPS", state.m_windY_MPS },
{ "m-windZ-MPS", state.m_windZ_MPS },
{ "m-propRPM", state.m_propRPM },
{ "m-heliMainRotorRPM", state.m_heliMainRotorRPM },
{ "m-batteryVoltage-VOLTS", state.m_batteryVoltage_VOLTS },
{ "m-batteryCurrentDraw-AMPS", state.m_batteryCurrentDraw_AMPS },
{ "m-batteryRemainingCapacity-MAH", state.m_batteryRemainingCapacity_MAH },
{ "m-fuelRemaining-OZ", state.m_fuelRemaining_OZ },
{ "m-isLocked", state.m_isLocked },
{ "m-hasLostComponents", state.m_hasLostComponents },
{ "m-anEngineIsRunning", state.m_anEngineIsRunning },
{ "m-isTouchingGround", state.m_isTouchingGround },
{ "m-currentAircraftStatus", state.m_currentAircraftStatus },
{ "m-currentPhysicsTime-SEC", state.m_currentPhysicsTime_SEC },
{ "m-currentPhysicsSpeedMultiplier", state.m_currentPhysicsSpeedMultiplier },
{ "m-orientationQuaternion-X", state.m_orientationQuaternion_X },
{ "m-orientationQuaternion-Y", state.m_orientationQuaternion_Y },
{ "m-orientationQuaternion-Z", state.m_orientationQuaternion_Z },
{ "m-orientationQuaternion-W", state.m_orientationQuaternion_W },
{ "m-flightAxisControllerIsActive", state.m_flightAxisControllerIsActive },
{ "m-resetButtonHasBeenPressed", state.m_resetButtonHasBeenPressed },
};
private:
char *soap_request(const char *action, const char *fmt, ...);
void exchange_data(const struct sitl_input &input);
void parse_reply(const char *reply);
double initial_time_s = 0;
double last_time_s = 0;
bool heli_demix = false;
bool rev4_servos = false;
bool controller_started = false;
uint64_t frame_counter = 0;
uint64_t activation_frame_counter = 0;
double last_frame_count_s = 0;
Vector3f position_offset;
Vector3f last_velocity_ef;
Matrix3f att_rotation;
enum Rotation rotation = ROTATION_NONE;
const char *controller_ip = "127.0.0.1";
uint16_t controller_port = 18083;
};
} // namespace SITL