/**
 ******************************************************************************
 *
 * @file       hitlnoisegeneration.cpp
 * @author     The OpenPilot Team, http://www.openpilot.org Copyright (C) 2012.
 * @brief
 * @see        The GNU Public License (GPL) Version 3
 * @defgroup   hitlplugin
 * @{
 *
 *****************************************************************************/
/*
 * 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
 */

#include "hitlnoisegeneration.h"


HitlNoiseGeneration::HitlNoiseGeneration()
{
    memset(&noise, 0, sizeof(Noise));
}


HitlNoiseGeneration::~HitlNoiseGeneration()
{}

Noise HitlNoiseGeneration::getNoise()
{
    return noise;
}

Noise HitlNoiseGeneration::generateNoise()
{
    noise.accelStateData.x       = 0;
    noise.accelStateData.y       = 0;
    noise.accelStateData.z       = 0;

    noise.gpsPosData.Latitude    = 0;
    noise.gpsPosData.Longitude   = 0;
    noise.gpsPosData.Groundspeed = 0;
    noise.gpsPosData.Heading     = 0;
    noise.gpsPosData.Altitude    = 0;

    noise.gpsVelData.North       = 0;
    noise.gpsVelData.East = 0;
    noise.gpsVelData.Down = 0;

    noise.baroAltData.Altitude = 0;

    noise.attStateData.Roll    = 0;
    noise.attStateData.Pitch   = 0;
    noise.attStateData.Yaw     = 0;

    noise.gyroStateData.x  = 0;
    noise.gyroStateData.y  = 0;
    noise.gyroStateData.z  = 0;

    noise.accelStateData.x = 0;
    noise.accelStateData.y = 0;
    noise.accelStateData.z = 0;

    noise.airspeedState.CalibratedAirspeed = 0;

    return noise;
}