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Satellites
src
gSatWrapper.hpp
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/***************************************************************************
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* Name: gSatStelWrapper.hpp
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*
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* Description: Wrapper over gSatTEME class.
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* This class allow use Satellite orbit calculation module (gSAt) in
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* Stellarium 'native' mode using Stellarium objects.
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*
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***************************************************************************/
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/***************************************************************************
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* Copyright (C) 2006 by J.L. Canales *
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* jlcanales.gasco@gmail.com *
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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 2 of the License, or *
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* (at your option) any later version. *
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* *
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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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* *
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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, write to the *
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* Free Software Foundation, Inc., *
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* 51 Franklin Street, Suite 500, Boston, MA 02110-1335, USA. *
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***************************************************************************/
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#ifndef _GSATWRAPPER_HPP_
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#define _GSATWRAPPER_HPP_ 1
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#include <QString>
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#include "VecMath.hpp"
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#include "gsatellite/gSatTEME.hpp"
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#include "gsatellite/gTime.hpp"
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//constants for predict visibility
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#define RADAR_SUN 1
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#define VISIBLE 2
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#define RADAR_NIGHT 3
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#define NOT_VISIBLE 4
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class
gSatWrapper
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{
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public
:
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gSatWrapper
(QString designation, QString tle1,QString tle2);
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~
gSatWrapper
();
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// Operation updateEpoch
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void
updateEpoch
();
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void
setEpoch(
double
ai_julianDaysEpoch);
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// Operation getTEMEPos
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Vec3d
getTEMEPos
();
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// Operation getTEMEVel
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Vec3d
getTEMEVel
();
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// Operation: getSubPoint
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Vec3d
getSubPoint
();
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// Operation getAltAz
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Vec3d
getAltAz
();
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// Operation getSlantRange
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void
getSlantRange
(
double
&ao_slantRange,
double
&ao_slantRangeRate);
//meassured in km and km/s
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// Operation getVisibilityPredict
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int
getVisibilityPredict
();
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private
:
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// Operation calcObserverECIPosition
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void
calcObserverECIPosition(
Vec3d
& ao_position,
Vec3d
& ao_vel);
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private
:
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gSatTEME
*pSatellite;
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gTime
epoch;
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};
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#endif
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