ardupilot/libraries/SITL/SIM_EFI_MegaSquirt.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/>.
*/
/*
simulate MegaSquirt EFI system
./Tools/autotest/sim_vehicle.py --gdb --debug -v ArduPlane -A --uartF=sim:megasquirt --speedup=1
param set SERIAL5_PROTOCOL 24
param set SIM_EFI_TYPE 1
param set EFI_TYPE 1
reboot
status EFI_STATUS
./Tools/autotest/autotest.py --gdb --debug build.Plane test.Plane.MegaSquirt
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*/
#pragma once
#include <SITL/SITL.h>
#include <AP_HAL/utility/Socket.h>
#include "SIM_SerialDevice.h"
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namespace SITL {
class EFI_MegaSquirt : public SerialDevice {
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public:
using SerialDevice::SerialDevice;
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void update();
private:
void send_table();
struct PACKED {
uint16_t size;
uint8_t command;
uint8_t CANid;
uint8_t table;
uint16_t table_offset;
uint16_t table_size;
uint32_t crc;
} r_command;
uint8_t *buf = (uint8_t *)&r_command;
uint8_t ofs;
struct PACKED {
uint16_t uptime_s;
uint16_t pulseWidth1_us;
uint16_t pulseWidth2_us;
uint16_t rpm;
int16_t advance_cdeg;
int8_t squirt;
int8_t engine_status;
uint8_t afr_target1;
uint8_t afr_target2;
uint8_t wbo2_en1;
uint8_t wbo2_en2;
int16_t baro_hPa;
int16_t map_hPa;
int16_t mat_cF;
int16_t ct_cF;
int16_t throttle_pos;
int16_t afr1;
int16_t afr2;
int16_t knock;
int16_t egocor1;
int16_t egocor2;
int16_t aircor;
int16_t warmcor;
int16_t accel_enrich;
int16_t tps_fuel_cut;
int16_t baroCorrection;
int16_t gammaEnrich;
int16_t ve1;
int16_t ve2;
int16_t iacstep;
int16_t cold_adv_deg;
int16_t TPSdot;
int16_t MAPdot;
int16_t dwell;
int16_t MAF;
uint8_t fuelload;
uint8_t pad[128-67];
uint16_t fuelPressure;
} table7;
float tps;
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};
}