mirror of https://github.com/ArduPilot/ardupilot
81 lines
2.2 KiB
C
81 lines
2.2 KiB
C
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/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
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/*
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This program is free software: you can redistribute it and/or modify
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it under the terms of the GNU General Public License as published by
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the Free Software Foundation, either version 3 of the License, or
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(at your option) any later version.
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This program is distributed in the hope that it will be useful,
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but WITHOUT ANY WARRANTY; without even the implied warranty of
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MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
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GNU General Public License for more details.
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You should have received a copy of the GNU General Public License
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along with this program. If not, see <http://www.gnu.org/licenses/>.
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*/
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/*
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simulator connection for ardupilot version of CRRCSim
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*/
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#ifndef _SIM_CRRCSIM_H
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#define _SIM_CRRCSIM_H
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#include "SIM_Aircraft.h"
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#include <utility/Socket.h>
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/*
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a CRRCSim simulator
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*/
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class CRRCSim : public Aircraft
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{
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public:
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CRRCSim(const char *home_str, const char *frame_str);
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/* update model by one time step */
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void update(const struct sitl_input &input);
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/* static object creator */
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static Aircraft *create(const char *home_str, const char *frame_str) {
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return new CRRCSim(home_str, frame_str);
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}
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private:
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/*
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packet sent to CRRCSim
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*/
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struct servo_packet {
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float roll_rate;
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float pitch_rate;
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float throttle;
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float yaw_rate;
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float col_pitch;
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};
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/*
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reply packet sent from CRRCSim to ArduPilot
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*/
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struct fdm_packet {
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double timestamp;
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double latitude, longitude;
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double altitude;
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double heading;
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double speedN, speedE, speedD;
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double xAccel, yAccel, zAccel;
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double rollRate, pitchRate, yawRate;
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double roll, pitch, yaw;
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double airspeed;
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};
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void send_servos_heli(const struct sitl_input &input);
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void send_servos_fixed_wing(const struct sitl_input &input);
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void recv_fdm(const struct sitl_input &input);
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void send_servos(const struct sitl_input &input);
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bool heli_servos;
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double last_timestamp;
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SocketAPM sock;
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};
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#endif // _SIM_CRRCSIM_H
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