mirror of
https://github.com/swift-project/pilotclient.git
synced 2026-03-31 21:15:33 +08:00
32f60722c8
* removed unused samples / tests * fixed found Doxygen issues * removed blacksimfreefunctions, now in BlackMisc::Simulation::registerMetadata() * samples_vetcor_geo to samples_geo
273 lines
12 KiB
C++
273 lines
12 KiB
C++
/* Copyright (C) 2013 VATSIM Community / contributors
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* This Source Code Form is subject to the terms of the Mozilla Public
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* License, v. 2.0. If a copy of the MPL was not distributed with this
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* file, You can obtain one at http://mozilla.org/MPL/2.0/. */
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#ifndef NOMINMAX
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#define NOMINMAX
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#endif
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#include "fsuipc.h"
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#include <Windows.h>
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// bug in FSUIPC_User.h, windows.h not included, so we have to import it first
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#include "FSUIPC/FSUIPC_User.h"
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#include "blackmisc/simulation/fscommon/bcdconversions.h"
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#include "blackmisc/logmessage.h"
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#include <QDebug>
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#include <QLatin1Char>
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#include <QDateTime>
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using namespace BlackMisc;
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using namespace BlackMisc::Simulation::FsCommon;
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using namespace BlackMisc::Aviation;
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using namespace BlackMisc::Network;
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using namespace BlackMisc::Geo;
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using namespace BlackMisc::Simulation;
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using namespace BlackMisc::PhysicalQuantities;
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namespace BlackSimPlugin
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{
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namespace FsCommon
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{
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CFsuipc::CFsuipc() { }
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CFsuipc::~CFsuipc()
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{
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this->disconnect();
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}
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bool CFsuipc::connect()
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{
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DWORD result;
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this->m_lastErrorMessage = "";
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if (this->m_connected) return this->m_connected; // already connected
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if (FSUIPC_Open(SIM_ANY, &result))
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{
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this->m_connected = true;
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int simIndex = static_cast<int>(FSUIPC_FS_Version);
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QString sim(
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(simIndex >= 0 && simIndex < CFsuipc::simulators().size()) ?
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CFsuipc::simulators().at(simIndex) :
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"Unknown FS");
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QString ver("%1.%2.%3.%4%5");
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ver = ver.arg(QLatin1Char(48 + (0x0f & (FSUIPC_Version >> 28))))
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.arg(QLatin1Char(48 + (0x0f & (FSUIPC_Version >> 24))))
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.arg(QLatin1Char(48 + (0x0f & (FSUIPC_Version >> 20))))
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.arg(QLatin1Char(48 + (0x0f & (FSUIPC_Version >> 16))))
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.arg((FSUIPC_Version & 0xffff) ? "a" + (FSUIPC_Version & 0xff) - 1 : "");
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this->m_fsuipcVersion = QString("FSUIPC %1 (%2)").arg(ver).arg(sim);
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// CLogMessage(this).info("FSUIPC connected: %1") << this->m_fsuipcVersion;
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}
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else
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{
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this->m_connected = false;
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int index = static_cast<int>(result);
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this->m_lastErrorMessage = CFsuipc::errorMessages().at(index);
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CLogMessage(this).info("FSUIPC not connected: %1") << this->m_lastErrorMessage;
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}
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return this->m_connected;
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}
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void CFsuipc::disconnect()
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{
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FSUIPC_Close(); // Closing when it wasn't open is okay, so this is safe here
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this->m_connected = false;
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}
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bool CFsuipc::write(const CSimulatedAircraft &aircraft)
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{
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if (!this->isConnected()) { return false; }
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Q_UNUSED(aircraft);
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//! \todo FSUIPC write values
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return false;
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}
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bool CFsuipc::read(CSimulatedAircraft &aircraft, bool cockpit, bool situation, bool aircraftParts)
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{
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DWORD dwResult;
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char localFsTimeRaw[3];
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char modelNameRaw[256];
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qint16 com1ActiveRaw = 0, com2ActiveRaw = 0, com1StandbyRaw = 0, com2StandbyRaw = 0;
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qint16 transponderCodeRaw = 0;
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qint8 xpdrModeSb3Raw = 0, xpdrIdentSb3Raw = 0;
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qint32 groundspeedRaw = 0, pitchRaw = 0, bankRaw = 0, headingRaw = 0;
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qint64 altitudeRaw = 0;
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qint32 groundAltitudeRaw = 0;
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qint64 latitudeRaw = 0, longitudeRaw = 0;
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qint16 lightsRaw = 0;
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qint16 onGroundRaw = 0;
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qint32 flapsControlRaw = 0, gearControlRaw = 0, spoilersControlRaw = 0;
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qint16 numberOfEngines = 0;
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qint16 engine1CombustionFlag = 0, engine2CombustionFlag = 0, engine3CombustionFlag = 0, engine4CombustionFlag = 0;
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// http://www.projectmagenta.com/all-fsuipc-offsets/
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// https://www.ivao.aero/softdev/ivap/fsuipc_sdk.asp
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// http://squawkbox.ca/doc/sdk/fsuipc.php
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if (!this->isConnected()) { return false; }
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if (!(aircraftParts || situation || cockpit)) { return false; }
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bool read = false;
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bool cockpitN = !cockpit;
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bool situationN = !situation;
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bool aircraftPartsN = ! aircraftParts;
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if (FSUIPC_Read(0x0238, 3, localFsTimeRaw, &dwResult) &&
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// COM settings
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(cockpitN || FSUIPC_Read(0x034e, 2, &com1ActiveRaw, &dwResult)) &&
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(cockpitN || FSUIPC_Read(0x3118, 2, &com2ActiveRaw, &dwResult)) &&
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(cockpitN || FSUIPC_Read(0x311a, 2, &com1StandbyRaw, &dwResult)) &&
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(cockpitN || FSUIPC_Read(0x311c, 2, &com2StandbyRaw, &dwResult)) &&
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(cockpitN || FSUIPC_Read(0x0354, 2, &transponderCodeRaw, &dwResult)) &&
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// COM Settings, transponder, SB3
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(cockpitN || FSUIPC_Read(0x7b91, 1, &xpdrModeSb3Raw, &dwResult)) &&
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(cockpitN || FSUIPC_Read(0x7b93, 1, &xpdrIdentSb3Raw, &dwResult)) &&
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// Speeds, situation
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(situationN || FSUIPC_Read(0x02b4, 4, &groundspeedRaw, &dwResult)) &&
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(situationN || FSUIPC_Read(0x0578, 4, &pitchRaw, &dwResult)) &&
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(situationN || FSUIPC_Read(0x057c, 4, &bankRaw, &dwResult)) &&
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(situationN || FSUIPC_Read(0x0580, 4, &headingRaw, &dwResult)) &&
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(situationN || FSUIPC_Read(0x0570, 8, &altitudeRaw, &dwResult)) &&
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// Position
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(situationN || FSUIPC_Read(0x0560, 8, &latitudeRaw, &dwResult)) &&
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(situationN || FSUIPC_Read(0x0568, 8, &longitudeRaw, &dwResult)) &&
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(situationN || FSUIPC_Read(0x0020, 4, &groundAltitudeRaw, &dwResult)) &&
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// model name
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(aircraftPartsN || FSUIPC_Read(0x3d00, 256, &modelNameRaw, &dwResult)) &&
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// aircraft parts
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(aircraftPartsN || FSUIPC_Read(0x0D0C, 2, &lightsRaw, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x0366, 2, &onGroundRaw, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x0BDC, 4, &flapsControlRaw, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x0BE8, 4, &gearControlRaw, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x0BD0, 4, &spoilersControlRaw, &dwResult)) &&
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// engines
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(aircraftPartsN || FSUIPC_Read(0x0AEC, 2, &numberOfEngines, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x0894, 2, &engine1CombustionFlag, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x092C, 2, &engine2CombustionFlag, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x09C4, 2, &engine3CombustionFlag, &dwResult)) &&
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(aircraftPartsN || FSUIPC_Read(0x0A5C, 2, &engine4CombustionFlag, &dwResult)) &&
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// If we wanted other reads/writes at the same time, we could put them here
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FSUIPC_Process(&dwResult))
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{
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read = true;
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// time, basically as a heartbeat
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QString fsTime;
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fsTime.sprintf("%02d:%02d:%02d", localFsTimeRaw[0], localFsTimeRaw[1], localFsTimeRaw[2]);
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if (cockpit)
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{
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// COMs
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CComSystem com1 = aircraft.getCom1System();
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CComSystem com2 = aircraft.getCom2System();
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CTransponder xpdr = aircraft.getTransponder();
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// 2710 => 12710 => / 100.0 => 127.1
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com1ActiveRaw = (10000 + CBcdConversions::bcd2Dec(com1ActiveRaw));
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com2ActiveRaw = (10000 + CBcdConversions::bcd2Dec(com2ActiveRaw));
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com1StandbyRaw = (10000 + CBcdConversions::bcd2Dec(com1StandbyRaw));
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com2StandbyRaw = (10000 + CBcdConversions::bcd2Dec(com2StandbyRaw));
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com1.setFrequencyActiveMHz(com1ActiveRaw / 100.0);
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com2.setFrequencyActiveMHz(com2ActiveRaw / 100.0);
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com1.setFrequencyStandbyMHz(com1StandbyRaw / 100.0);
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com2.setFrequencyStandbyMHz(com2StandbyRaw / 100.0);
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transponderCodeRaw = static_cast<qint16>(CBcdConversions::bcd2Dec(transponderCodeRaw));
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xpdr.setTransponderCode(transponderCodeRaw);
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// Mode by SB3
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if (xpdrIdentSb3Raw != 0)
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{
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//! \todo Reset value for FSUIPC
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xpdr.setTransponderMode(CTransponder::StateIdent);
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}
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else
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{
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xpdr.setTransponderMode(
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xpdrModeSb3Raw == 0 ? CTransponder::ModeC : CTransponder::StateStandby
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);
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}
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aircraft.setCockpit(com1, com2, xpdr);
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} // cockpit
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if (situation)
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{
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// position
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const double latCorrectionFactor = 90.0 / (10001750.0 * 65536.0 * 65536.0);
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const double lonCorrectionFactor = 360.0 / (65536.0 * 65536.0 * 65536.0 * 65536.0);
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CAircraftSituation situation = aircraft.getSituation();
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CCoordinateGeodetic position = situation.getPosition();
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CLatitude lat(latitudeRaw * latCorrectionFactor, CAngleUnit::deg());
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CLongitude lon(longitudeRaw * lonCorrectionFactor, CAngleUnit::deg());
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CLength groundAltitude(groundAltitudeRaw / 256.0, CLengthUnit::m());
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position.setLatitude(lat);
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position.setLongitude(lon);
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position.setGeodeticHeight(groundAltitude);
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situation.setPosition(position);
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// speeds, situation
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const double angleCorrectionFactor = 360.0 / 65536.0 / 65536.0; // see FSUIPC docu
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CAngle pitch = CAngle(pitchRaw * angleCorrectionFactor, CAngleUnit::deg());
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CAngle bank = CAngle(bankRaw * angleCorrectionFactor, CAngleUnit::deg());
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CHeading heading = CHeading(headingRaw * angleCorrectionFactor, CHeading::True, CAngleUnit::deg());
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CSpeed groundspeed(groundspeedRaw / 65536.0, CSpeedUnit::m_s());
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CAltitude altitude(altitudeRaw / (65536.0 * 65536.0), CAltitude::MeanSeaLevel, CLengthUnit::m());
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situation.setBank(bank);
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situation.setHeading(heading);
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situation.setPitch(pitch);
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situation.setGroundspeed(groundspeed);
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situation.setAltitude(altitude);
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aircraft.setSituation(situation);
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} // situation
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if (aircraftParts)
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{
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// model
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const QString modelName = QString(modelNameRaw); // to be used to distinguish offsets for different models
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aircraft.setModelString(modelName);
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CAircraftLights lights(lightsRaw & (1 << 4), lightsRaw & (1 << 2), lightsRaw & (1 << 3), lightsRaw & (1 << 1),
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lightsRaw & (1 << 0), lightsRaw & (1 << 8));
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QList<bool> helperList { engine1CombustionFlag != 0, engine2CombustionFlag != 0,
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engine3CombustionFlag != 0, engine4CombustionFlag != 0
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};
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CAircraftEngineList engines;
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for (int index = 0; index < numberOfEngines; ++index)
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{
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engines.push_back(CAircraftEngine(index + 1, helperList.at(index)));
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}
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CAircraftParts parts(lights, gearControlRaw == 16383, flapsControlRaw * 100 / 16383,
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spoilersControlRaw == 16383, engines, onGroundRaw == 1);
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aircraft.setParts(parts);
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} // parts
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} // read
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return read;
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}
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double CFsuipc::intToFractional(double fractional)
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{
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double f = fractional / 10.0;
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if (f < 1.0) return f;
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return intToFractional(f);
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}
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} // namespace
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} // namespace
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