/**
 ******************************************************************************
 *
 * @file       aerosimrcdatastruct.h
 * @author     The OpenPilot Team, http://www.openpilot.org Copyright (C) 2010-2012.
 * @addtogroup 3rdParty Third-party integration
 * @{
 * @addtogroup AeroSimRC AeroSimRC proxy plugin
 * @{
 * @brief AeroSimRC simulator to HITL proxy plugin
 *****************************************************************************/
/*
 * 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, write to the Free Software Foundation, Inc.,
 * 59 Temple Place, Suite 330, Boston, MA 02111-1307 USA
 */

#ifndef AEROSIMRCDATASTRUCT_H
#define AEROSIMRCDATASTRUCT_H

#include <QtCore>

const quint8 AEROSIMRC_MAX_CHANNELS = 39;
const quint16 DBG_BUFFER_MAX_SIZE   = 4096;

#define MAX_DLL_USER_MENU_ITEMS 16
#define OBSOLETE_MIT_COMMAND    (1 << 0)
#define OBSOLETE_MIT_CHECKBOX   (1 << 1)
#define OBSOLETE_MIT_SEPARATOR  (1 << 7)

#define PACK_STRUCT             __attribute__((packed))

struct simToPlugin {
    quint16    structSize;
    float      simTimeStep;
    float      chSimTX[AEROSIMRC_MAX_CHANNELS];
    float      chSimRX[AEROSIMRC_MAX_CHANNELS];
    uchar      *OSDVideoBuf;
    quint32    simMenuStatus;
    float      initPosX;
    float      initPosY;
    float      initPosZ;
    float      initHeading;
    float      initPitch;
    float      initRoll;
    float      wpHomeX;
    float      wpHomeY;
    float      wpHomeLat;
    float      wpHomeLong;
    const char *wpHomeDesc; // (m, deg, string)
    float      wpAX;
    float      wpAY;
    float      wpALat;
    float      wpALong;
    const char *wpADesc; // (m, deg, string)
    float      wpBX;
    float      wpBY;
    float      wpBLat;
    float      wpBLong;
    const char *wpBDesc; // (m, deg, string)
    float      wpCX;
    float      wpCY;
    float      wpCLat;
    float      wpCLong;
    const char *wpCDesc; // (m, deg, string)
    float      wpDX;
    float      wpDY;
    float      wpDLat;
    float      wpDLong;
    const char *wpDDesc; // (m, deg, string)
    float      posX;
    float      posY;
    float      posZ;
    float      velX;
    float      velY;
    float      velZ;
    float      angVelX;
    float      angVelY;
    float      angVelZ;
    float      accelX;
    float      accelY;
    float      accelZ;
    qreal      latitude;
    qreal      longitude;
    float      AGL;
    float      heading;
    float      pitch;
    float      roll;
    float      windVelX;
    float      windVelY;
    float      windVelZ;
    float      eng1RPM;
    float      eng2RPM;
    float      eng3RPM;
    float      eng4RPM;
    float      voltage;          // V
    float      current;          // A
    float      consumedCharge;   // Ah
    float      capacity;         // Ah
    float      fuelConsumed;     // l
    float      fuelTankCapacity; // l
    // ver 3.83
    qint16     screenW;
    qint16     screenH;
    // Model Orientation Matrix (X=Right, Y=Front, Z=Up)
    float      axisXx;
    float      axisXy;
    float      axisXz;
    float      axisYx;
    float      axisYy;
    float      axisYz;
    float      axisZx;
    float      axisZy;
    float      axisZz;
    // Model data in body frame coordinates (X=Right, Y=Front, Z=Up)
    float      velXm;    // m/s   Model velocity in body coordinates
    float      velYm;
    float      velZm;
    float      angVelXm; // rad/s Model angular velocity in body coordinates
    float      angVelYm;
    float      angVelZm;
    float      accelXm;  // m/s/s Model acceleration in body coordinates
    float      accelYm;
    float      accelZm;
    // ver 3.90
    quint32    OSDVideoBufSize;
} PACK_STRUCT; // normal - 592, packed - 582 OK (3.81)
               // normal - ???, packed - 658 OK (3.83)
               // normal - ???, packed - 662 OK (3.90)

struct pluginToSim {
    quint16    structSize;
    const char *dbgInfoText;
    uchar   chOverTX[AEROSIMRC_MAX_CHANNELS];
    float   chNewTX[AEROSIMRC_MAX_CHANNELS];
    uchar   chOverRX[AEROSIMRC_MAX_CHANNELS];
    float   chNewRX[AEROSIMRC_MAX_CHANNELS];
    float   newPosX;      // m
    float   newPosY;
    float   newPosZ;
    float   newVelX;      // m/s
    float   newVelY;
    float   newVelZ;
    float   newAngVelX;   // rad/s
    float   newAngVelY;
    float   newAngVelZ;
    float   newHeading;   // rad
    float   newPitch;
    float   newRoll;
    quint32 modelOverrideFlags;
    quint32 newMenuStatus;
    quint8  isOSDShow;
    quint8  isOSDChanged;
    quint16 OSDWindow_DX;
    quint16 OSDWindow_DY;
    float   OSDScale;
    float   newWindVelX;
    float   newWindVelY;
    float   newWindVelZ;
    float   newEng1RPM;
    float   newEng2RPM;
    float   newEng3RPM;
    float   newEng4RPM;
    float   newVoltage;
    float   newCurrent;
    float   newConsumedCharge;
    float   newFuelConsumed;
    quint8  modelCrashInhibit;
    // ver 3.83
    qint16  newScreenW;     // Simulator window position and size on screen
    qint16  newScreenH;
    qint16  newScreenX;
    qint16  newScreenY;
} PACK_STRUCT; // normal 516, packed 507 OK (3.81)
               // normal ???, packed 515 OK (3.83 & 3.90)

struct TPluginMenuItem {
    quint32 OBSOLETE_eType;
    char    *OBSOLETE_strName;
} PACK_STRUCT;

struct pluginInit {
    quint32    nStructSize;
    char       *OBSOLETE_strMenuTitle;
    TPluginMenuItem OBSOLETE_atMenuItem[MAX_DLL_USER_MENU_ITEMS];
    const char *strPluginFolder;
    const char *strOutputFolder;
} PACK_STRUCT; // normal - 144, packed - 144 OK (3.81 & 3.83 & 3.90)

#undef PACK_STRUCT

#endif // AEROSIMRCDATASTRUCT_H
