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/******************************************************************************
*
* Purpose: Support for storing and manipulating Toutin information
*
******************************************************************************
* Copyright (c) 2009
* PCI Geomatics, 50 West Wilmot Street, Richmond Hill, Ont, Canada
*
* Permission is hereby granted, free of charge, to any person obtaining a
* copy of this software and associated documentation files (the "Software"),
* to deal in the Software without restriction, including without limitation
* the rights to use, copy, modify, merge, publish, distribute, sublicense,
* and/or sell copies of the Software, and to permit persons to whom the
* Software is furnished to do so, subject to the following conditions:
*
* The above copyright notice and this permission notice shall be included
* in all copies or substantial portions of the Software.
*
* THE SOFTWARE IS PROVIDED "AS IS", WITHOUT WARRANTY OF ANY KIND, EXPRESS
* OR IMPLIED, INCLUDING BUT NOT LIMITED TO THE WARRANTIES OF MERCHANTABILITY,
* FITNESS FOR A PARTICULAR PURPOSE AND NONINFRINGEMENT. IN NO EVENT SHALL
* THE AUTHORS OR COPYRIGHT HOLDERS BE LIABLE FOR ANY CLAIM, DAMAGES OR OTHER
* LIABILITY, WHETHER IN AN ACTION OF CONTRACT, TORT OR OTHERWISE, ARISING
* FROM, OUT OF OR IN CONNECTION WITH THE SOFTWARE OR THE USE OR OTHER
* DEALINGS IN THE SOFTWARE.
****************************************************************************/
#ifndef __INCLUDE_PCIDSK_TOUTIN_INFORMATION_H
#define __INCLUDE_PCIDSK_TOUTIN_INFORMATION_H
#include "segment/orbitstructures.h"
namespace PCIDSK
{
/* -------------------------------------------------------------------- */
/* SRITInfo_t - Satellite Model structure. */
/* -------------------------------------------------------------------- */
#define AP_MDL 1
#define SRIT_MDL 2
#define RF_MDL 6
#define RTCS_MDL 7
#define ADS_MDL 9
#define SRITModele 0
#define SRITModele1A 1
#define SRITModele1B 2
#define SRITModeleSAR 3
#define SRITModele1AHR 4
#define SRITModeleEros 5
#define MAX_SPOT_LINES 30000
/**
* the SRITInfo_t struct contains all information
* for the Toutin Math Model.
*/
struct SRITInfo_t
{
/**
* default constructor
*/
SRITInfo_t()
{
OrbitPtr = NULL;
}
/**
* destructor
*/
~SRITInfo_t()
{
delete OrbitPtr;
}
/**
* Copy constructor.
* @param oSI the SRITInfo_t to copy
*/
SRITInfo_t(const SRITInfo_t& oSI)
{
OrbitPtr = NULL;
Copy(oSI);
}
/**
* Assignment operator
* @param oSI the SRITInfo_t to assign
*/
SRITInfo_t& operator=(const SRITInfo_t& oSI)
{
Copy(oSI);
return *this;
}
/**
* Copy function
* @param oSI the SRITInfo_t to copy
*/
void Copy(const SRITInfo_t& oSI)
{
if(this == &oSI)
{
return;
}
delete OrbitPtr;
OrbitPtr = NULL;
if(oSI.OrbitPtr)
{
OrbitPtr = new EphemerisSeg_t(*oSI.OrbitPtr);
}
for(int i=0 ; i<256 ; i++)
{
nGCPIds[i] = oSI.nGCPIds[i];
nPixel[i] = oSI.nPixel[i];
nLine[i] = oSI.nLine[i];
dfElev[i] = oSI.dfElev[i];
}
N0x2 = oSI.N0x2;
aa = oSI.aa;
SmALPHA = oSI.SmALPHA;
bb = oSI.bb;
C0 = oSI.C0;
cc = oSI.cc;
COS_KHI = oSI.COS_KHI;
DELTA_GAMMA = oSI.DELTA_GAMMA;
GAMMA = oSI.GAMMA;
K_1 = oSI.K_1;
L0 = oSI.L0;
P = oSI.P;
Q = oSI.Q;
TAU = oSI.TAU;
THETA = oSI.THETA;
THETA_SEC = oSI.THETA_SEC;
X0 = oSI.X0;
Y0 = oSI.Y0;
delh = oSI.delh;
COEF_Y2 = oSI.COEF_Y2;
delT = oSI.delT;
delL = oSI.delL;
delTau = oSI.delTau;
nDownSample = oSI.nDownSample;
nGCPCount = oSI.nGCPCount;
nEphemerisSegNo = oSI.nEphemerisSegNo;
nAttitudeFlag = oSI.nAttitudeFlag;
utmunit = oSI.utmunit;
GCPUnit = oSI.GCPUnit;
GCPMeanHtFlag = oSI.GCPMeanHtFlag;
dfGCPMeanHt = oSI.dfGCPMeanHt;
dfGCPMinHt = oSI.dfGCPMinHt;
dfGCPMaxHt = oSI.dfGCPMaxHt;
Qdeltar = oSI.Qdeltar;
Hdeltat = oSI.Hdeltat;
Sensor = oSI.Sensor;
nSensor = oSI.nSensor;
nModel = oSI.nModel;
RawToGeo = oSI.RawToGeo;
oProjectionInfo = oSI.oProjectionInfo;
}
double N0x2;
double aa;
double SmALPHA;
double bb;
double C0;
double cc;
double COS_KHI;
double DELTA_GAMMA;
double GAMMA;
double K_1;
double L0;
double P;
double Q;
double TAU;
double THETA;
double THETA_SEC;
double X0;
double Y0;
double delh;
double COEF_Y2;
double delT;
double delL;
double delTau;
int nDownSample;
int nGCPCount;
int nEphemerisSegNo;
int nAttitudeFlag;
std::string utmunit;
std::string GCPUnit;
char GCPMeanHtFlag;
double dfGCPMeanHt;
double dfGCPMinHt;
double dfGCPMaxHt;
int nGCPIds[256];
int nPixel[256],nLine[256];
double dfElev[256];
std::vector<double> Qdeltar;
std::vector<double> Hdeltat;
std::string Sensor;
int nSensor;
int nModel;
EphemerisSeg_t *OrbitPtr;
bool RawToGeo;
std::string oProjectionInfo;
} ;
}
#endif // __INCLUDE_PCIDSK_TOUTIN_INFORMATION_H
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