/****************************************************************************** * * Purpose: Implementation of the CPCIDSKToutinModelSegment class. * ****************************************************************************** * Copyright (c) 2009 * PCI Geomatics, 90 Allstate Parkway, Markham, Ontario, Canada. * * SPDX-License-Identifier: MIT ****************************************************************************/ #include "segment/cpcidsksegment.h" #include "core/pcidsk_utils.h" #include "segment/cpcidsktoutinmodel.h" #include "pcidsk_exception.h" #include "core/pcidsk_utils.h" #include #include #include #include #include using namespace PCIDSK; CPCIDSKToutinModelSegment::CPCIDSKToutinModelSegment(PCIDSKFile *fileIn, int segmentIn, const char *segment_pointer) : CPCIDSKEphemerisSegment(fileIn, segmentIn, segment_pointer,false) { loaded_ = false; mbModified = false; mpoInfo = nullptr; Load(); } CPCIDSKToutinModelSegment::~CPCIDSKToutinModelSegment() { delete mpoInfo; } /** * Get the SRITInfo_t structure from read from the segment. * @return the Toutin information structure. */ SRITInfo_t CPCIDSKToutinModelSegment::GetInfo() const { if (!mpoInfo) { const_cast(this)->Load(); if (!mpoInfo) { ThrowPCIDSKException("Unable to load toutin segment."); return SRITInfo_t(); } } return (*mpoInfo); } /** * Set the toutin information in the segment. The segment will be tag * as modified and will be synchronize on disk with the next call to * the function synchronize. * @param oInfo the toutin information. */ void CPCIDSKToutinModelSegment::SetInfo(const SRITInfo_t& oInfo) { if(&oInfo == mpoInfo) { return ; } if(mpoInfo) { delete mpoInfo; } mpoInfo = new SRITInfo_t(oInfo); mbModified = true; } /** * Load the contents of the segment */ void CPCIDSKToutinModelSegment::Load() { // Check if we've already loaded the segment into memory if (loaded_) { return; } seg_data.SetSize((int)data_size - 1024); ReadFromFile(seg_data.buffer, 0, data_size - 1024); if(seg_data.buffer_size == 0) { return; } SRITInfo_t* poInfo = BinaryToSRITInfo(); mpoInfo = poInfo; // We've now loaded the structure up with data. Mark it as being loaded // properly. loaded_ = true; } /** * Write the segment on disk */ void CPCIDSKToutinModelSegment::Write(void) { //We are not writing if nothing was loaded. if (!loaded_) { return; } SRITInfoToBinary(mpoInfo); WriteToFile(seg_data.buffer,0,seg_data.buffer_size); mbModified = false; } /** * Synchronize the segment, if it was modified then * write it into disk. */ void CPCIDSKToutinModelSegment::Synchronize() { if(mbModified) { this->Write(); } } /************************************************************************/ /* BinaryToSRITInfo() */ /************************************************************************/ /** * Translate a block of binary data into a SRIT segment. the caller is * responsible to free the returned memory with delete. * * @return Rational Satellite Model structure. */ SRITInfo_t * CPCIDSKToutinModelSegment::BinaryToSRITInfo() { int i,j,k,l; bool bVersion9; /* -------------------------------------------------------------------- */ /* Read the header block */ /* -------------------------------------------------------------------- */ // We test the name of the binary segment before starting to read // the buffer. if (!STARTS_WITH(seg_data.buffer, "MODEL ")) { seg_data.Put("MODEL ",0,8); return nullptr; // Something has gone terribly wrong! /*throw PCIDSKException("A segment that was previously " "identified as an RFMODEL " "segment does not contain the appropriate data. Found: [%s]", std::string(seg_data.buffer, 8).c_str());*/ } bVersion9 = false; int nVersion = seg_data.GetInt(8,1); if (nVersion == 9) { bVersion9 = true; } /* -------------------------------------------------------------------- */ /* Allocate the SRITModel. */ /* -------------------------------------------------------------------- */ std::unique_ptr SRITModel( new SRITInfo_t()); SRITModel->GCPMeanHtFlag = 0; SRITModel->nDownSample = 1; if(STARTS_WITH(seg_data.Get(22,2) , "DS")) { SRITModel->nDownSample = seg_data.GetInt(24,3); } /* -------------------------------------------------------------------- */ /* Read the Block 1 */ /* -------------------------------------------------------------------- */ SRITModel->N0x2 = seg_data.GetDouble(512,22); SRITModel->aa = seg_data.GetDouble(512+22,22); SRITModel->SmALPHA = seg_data.GetDouble(512+44,22); SRITModel->bb = seg_data.GetDouble(512+66,22); SRITModel->C0 = seg_data.GetDouble(512+88,22); SRITModel->cc = seg_data.GetDouble(512+110,22); SRITModel->COS_KHI = seg_data.GetDouble(512+132,22); SRITModel->DELTA_GAMMA = seg_data.GetDouble(512+154,22); SRITModel->GAMMA = seg_data.GetDouble(512+176,22); SRITModel->K_1 = seg_data.GetDouble(512+198,22); SRITModel->L0 = seg_data.GetDouble(512+220,22); SRITModel->P = seg_data.GetDouble(512+242,22); SRITModel->Q = seg_data.GetDouble(512+264,22); SRITModel->TAU = seg_data.GetDouble(512+286,22); SRITModel->THETA = seg_data.GetDouble(512+308,22); SRITModel->THETA_SEC = seg_data.GetDouble(512+330,22); SRITModel->X0 = seg_data.GetDouble(512+352,22); SRITModel->Y0 = seg_data.GetDouble(512+374,22); SRITModel->delh = seg_data.GetDouble(512+396,22); SRITModel->COEF_Y2 = seg_data.GetDouble(512+418,22); if (bVersion9) { SRITModel->delT = seg_data.GetDouble(512+440,22); SRITModel->delL = seg_data.GetDouble(512+462,22); SRITModel->delTau = seg_data.GetDouble(512+484,22); } else { SRITModel->delT = 0.0; SRITModel->delL = 0.0; SRITModel->delTau = 0.0; } /* -------------------------------------------------------------------- */ /* Read the GCP information in Block 2 */ /* -------------------------------------------------------------------- */ SRITModel->nGCPCount = seg_data.GetInt(2*512,10); if (SRITModel->nGCPCount > 256) SRITModel->nGCPCount = 256; SRITModel->nEphemerisSegNo = seg_data.GetInt(2*512+10,10); SRITModel->nAttitudeFlag = seg_data.GetInt(2*512+20,10); SRITModel->GCPUnit = seg_data.Get(2*512+30,16); SRITModel->dfGCPMeanHt = seg_data.GetDouble(2*512+50,22); SRITModel->dfGCPMinHt = seg_data.GetDouble(2*512+72,22); SRITModel->dfGCPMaxHt = seg_data.GetDouble(2*512+94,22); /* -------------------------------------------------------------------- */ /* Initialize a simple GeoTransform. */ /* -------------------------------------------------------------------- */ SRITModel->utmunit = seg_data.Get(2*512+225,16); if (std::strcmp(seg_data.Get(2*512+245,8),"ProjInfo")==0) { SRITModel->oProjectionInfo = seg_data.Get(2*512+255,256); } /* -------------------------------------------------------------------- */ /* Read the GCPs */ /* -------------------------------------------------------------------- */ l = 0; k = 4; for (j=0; jnGCPCount; j++) { SRITModel->nGCPIds[j] = seg_data.GetInt((k-1)*512+10*l,5); SRITModel->nPixel[j] = seg_data.GetInt((k-1)*512+10*(l+1),5); SRITModel->nLine[j] = seg_data.GetInt((k-1)*512+10*(l+1)+5,5); SRITModel->dfElev[j] = seg_data.GetInt((k-1)*512+10*(l+2),10); l+=3; if (l<50) continue; k++; l = 0; } /* -------------------------------------------------------------------- */ /* Call BinaryToEphemeris to get the orbital data */ /* -------------------------------------------------------------------- */ SRITModel->OrbitPtr = BinaryToEphemeris( 512*21 ); /* -------------------------------------------------------------------- */ /* Pass the sensor back to SRITModel */ /* -------------------------------------------------------------------- */ SRITModel->Sensor = SRITModel->OrbitPtr->SatelliteSensor; /* -------------------------------------------------------------------- */ /* Assign nSensor value */ /* -------------------------------------------------------------------- */ SRITModel->nSensor = GetSensor (SRITModel->OrbitPtr); SRITModel->nModel = GetModel (SRITModel->nSensor); if( SRITModel->nSensor == -999) { return (SRITInfo_t*)ThrowPCIDSKExceptionPtr("Invalid Sensor : %s.", SRITModel->OrbitPtr->SatelliteSensor.c_str()); } if( SRITModel->nModel == -999) { return (SRITInfo_t*)ThrowPCIDSKExceptionPtr("Invalid Model from sensor number: %d.", SRITModel->nSensor); } /* -------------------------------------------------------------------- */ /* Get the attitude data for SPOT */ /* -------------------------------------------------------------------- */ if (SRITModel->OrbitPtr->AttitudeSeg != nullptr || SRITModel->OrbitPtr->RadarSeg != nullptr) { AttitudeSeg_t *attitudeSeg = SRITModel->OrbitPtr->AttitudeSeg; if (SRITModel->OrbitPtr->Type == OrbAttitude && attitudeSeg != nullptr) { int ndata; ndata = attitudeSeg->NumberOfLine; for (i=0; iHdeltat.push_back( attitudeSeg->Line[i].ChangeInAttitude); SRITModel->Qdeltar.push_back( attitudeSeg->Line[i].ChangeEarthSatelliteDist); } } } else { SRITModel->Qdeltar.clear(); SRITModel->Hdeltat.clear(); } return SRITModel.release(); } /************************************************************************/ /* SRITInfoToBinary() */ /************************************************************************/ /** * Translate a SRITInfo_t into binary data. * Translate a SRITInfo_t into the corresponding block of * binary data. This function is expected to be used by * translators such as iisopen.c (VISTA) so that our satellite * models can be converted into some opaque serialized form. * Translate a Rpc Model into the corresponding block of binary data. * * @param SRITModel Satellite Model structure. */ void CPCIDSKToutinModelSegment::SRITInfoToBinary( SRITInfo_t *SRITModel ) { int i,j,k,l; double dfminht,dfmaxht,dfmeanht; int nPos = 0; /* -------------------------------------------------------------------- */ /* Create the data array. */ /* -------------------------------------------------------------------- */ seg_data.SetSize(512 * 21); //clean the buffer memset( seg_data.buffer , ' ', 512 * 21 ); /* -------------------------------------------------------------------- */ /* Initialize the header. */ /* -------------------------------------------------------------------- */ nPos = 512*0; seg_data.Put("MODEL 9.0",0,nPos+11); seg_data.Put("DS",nPos+22,2); seg_data.Put(SRITModel->nDownSample,nPos+24,3); /* -------------------------------------------------------------------- */ /* Write the model results to second segment */ /* -------------------------------------------------------------------- */ nPos = 512*1; seg_data.Put(SRITModel->N0x2,nPos,22,"%22.14f"); seg_data.Put(SRITModel->aa,nPos+22,22,"%22.14f"); seg_data.Put(SRITModel->SmALPHA,nPos+22*2,22,"%22.14f"); seg_data.Put(SRITModel->bb,nPos+22*3,22,"%22.14f"); seg_data.Put(SRITModel->C0,nPos+22*4,22,"%22.14f"); seg_data.Put(SRITModel->cc,nPos+22*5,22,"%22.14f"); seg_data.Put(SRITModel->COS_KHI,nPos+22*6,22,"%22.14f"); seg_data.Put(SRITModel->DELTA_GAMMA,nPos+22*7,22,"%22.14f"); seg_data.Put(SRITModel->GAMMA,nPos+22*8,22,"%22.14f"); seg_data.Put(SRITModel->K_1,nPos+22*9,22,"%22.14f"); seg_data.Put(SRITModel->L0,nPos+22*10,22,"%22.14f"); seg_data.Put(SRITModel->P,nPos+22*11,22,"%22.14f"); seg_data.Put(SRITModel->Q,nPos+22*12,22,"%22.14f"); seg_data.Put(SRITModel->TAU,nPos+22*13,22,"%22.14f"); seg_data.Put(SRITModel->THETA,nPos+22*14,22,"%22.14f"); seg_data.Put(SRITModel->THETA_SEC,nPos+22*15,22,"%22.14f"); seg_data.Put(SRITModel->X0,nPos+22*16,22,"%22.14f"); seg_data.Put(SRITModel->Y0,nPos+22*17,22,"%22.14f"); seg_data.Put(SRITModel->delh,nPos+22*18,22,"%22.14f"); seg_data.Put(SRITModel->COEF_Y2,nPos+22*19,22,"%22.14f"); seg_data.Put(SRITModel->delT,nPos+22*20,22,"%22.14f"); seg_data.Put(SRITModel->delL,nPos+22*21,22,"%22.14f"); seg_data.Put(SRITModel->delTau,nPos+22*22,22,"%22.14f"); /* -------------------------------------------------------------------- */ /* Find the min and max height */ /* -------------------------------------------------------------------- */ nPos = 2*512; if (SRITModel->nGCPCount > 256) SRITModel->nGCPCount = 256; if (SRITModel->nGCPCount != 0) { dfminht = 1.e38; dfmaxht = -1.e38; for (i=0; inGCPCount; i++) { if (SRITModel->dfElev[i] > dfmaxht) dfmaxht = SRITModel->dfElev[i]; if (SRITModel->dfElev[i] < dfminht) dfminht = SRITModel->dfElev[i]; } } else { dfminht = SRITModel->dfGCPMinHt; dfmaxht = 0; } dfmeanht = (dfminht + dfmaxht)/2.; seg_data.Put(SRITModel->nGCPCount,nPos,10); seg_data.Put("2",nPos+10,1); seg_data.Put("0",nPos+20,1); if (SRITModel->OrbitPtr->AttitudeSeg != nullptr || SRITModel->OrbitPtr->RadarSeg != nullptr || SRITModel->OrbitPtr->AvhrrSeg != nullptr ) { if (SRITModel->OrbitPtr->Type == OrbAttitude && SRITModel->OrbitPtr->AttitudeSeg != nullptr) { if (SRITModel->OrbitPtr->AttitudeSeg->NumberOfLine != 0) seg_data.Put("3",nPos+20,1); } } seg_data.Put(SRITModel->GCPUnit.c_str(),nPos+30,16); seg_data.Put("M",nPos+49,1); seg_data.Put(dfmeanht,nPos+50,22,"%22.14f"); seg_data.Put(dfminht,nPos+72,22,"%22.14f"); seg_data.Put(dfmaxht,nPos+94,22,"%22.14f"); seg_data.Put("NEWGCP",nPos+116,6); /* -------------------------------------------------------------------- */ /* Write the projection parameter if necessary */ /* -------------------------------------------------------------------- */ seg_data.Put(SRITModel->utmunit.c_str(),nPos+225,16); if(!SRITModel->oProjectionInfo.empty()) { seg_data.Put("ProjInfo: ",nPos+245,10); seg_data.Put(SRITModel->oProjectionInfo.c_str(), nPos+255,256); } /* -------------------------------------------------------------------- */ /* Write the GCP to third segment */ /* -------------------------------------------------------------------- */ nPos = 3*512; l = 0; k = 3; if (SRITModel->nGCPCount > 256) SRITModel->nGCPCount = 256; for (j=0; jnGCPCount; j++) { if (j > 255) break; seg_data.Put(SRITModel->nGCPIds[j],nPos+10*l,5); seg_data.Put((int)(SRITModel->nPixel[j]+0.5), nPos+10*(l+1),5); seg_data.Put((int)(SRITModel->nLine[j]+0.5), nPos+10*(l+1)+5,5); seg_data.Put((int)SRITModel->dfElev[j],nPos+10*(l+2),10); l+=3; if (l<50) continue; k++; nPos = 512*k; l = 0; } /* -------------------------------------------------------------------- */ /* Add the serialized form of the EphemerisSeg_t. */ /* -------------------------------------------------------------------- */ EphemerisToBinary( SRITModel->OrbitPtr , 512*21 ); } /** * Get the sensor enum from the orbit segment. * @param OrbitPtr the orbit segment * @return the sensor type. */ int CPCIDSKToutinModelSegment::GetSensor( EphemerisSeg_t *OrbitPtr) { int nSensor; nSensor = -999; if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "AVHRR")) nSensor = AVHRR; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PLA")) nSensor = PLA_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MLA")) nSensor = MLA_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ASTER")) nSensor = ASTER; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SAR")) { nSensor = SAR; if (OrbitPtr->PixelRes == 6.25) nSensor = RSAT_FIN; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-1")) nSensor = LISS_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-2")) nSensor = LISS_2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-3")) nSensor = LISS_3; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-L3-L2")) nSensor = LISS_L3_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-L3")) nSensor = LISS_L3; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-L4-L2")) nSensor = LISS_L4_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-L4")) nSensor = LISS_L4; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-P3-L2")) nSensor = LISS_P3_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-P3")) nSensor = LISS_P3; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-W3-L2")) nSensor = LISS_W3_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-W3")) nSensor = LISS_W3; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-M3")) nSensor = LISS_M3; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-AWF-L2")) nSensor = LISS_AWF_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "LISS-AWF")) nSensor = LISS_AWF; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "EOC")) nSensor = EOC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "IRS")) nSensor = IRS_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MSS")) nSensor = MSS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TM")) { nSensor = TM; if (OrbitPtr->PixelRes == 15) nSensor = ETM; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ETM")) nSensor = ETM; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "IKO")) { nSensor = IKO_PAN; if (OrbitPtr->PixelRes == 4) nSensor = IKO_MULTI; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ORBVIEW")) { nSensor = ORBVIEW_PAN; if (OrbitPtr->PixelRes == 4) nSensor = ORBVIEW_MULTI; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV3_PAN_BASIC")) nSensor = OV3_PAN_BASIC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV3_PAN_GEO")) nSensor = OV3_PAN_GEO; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV3_MULTI_BASIC")) nSensor = OV3_MULTI_BASIC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV3_MULTI_GEO")) nSensor = OV3_MULTI_GEO; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV5_PAN_BASIC")) nSensor = OV5_PAN_BASIC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV5_PAN_GEO")) nSensor = OV5_PAN_GEO; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV5_MULTI_BASIC")) nSensor = OV5_MULTI_BASIC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "OV5_MULTI_GEO")) nSensor = OV5_MULTI_GEO; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "QBIRD")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "QBIRD_PAN_STD")) nSensor = QBIRD_PAN_STD; // this checking must go first else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "QBIRD_PAN_STH")) nSensor = QBIRD_PAN_STH; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "QBIRD_PAN")) nSensor = QBIRD_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "QBIRD_MULTI_STD")) nSensor = QBIRD_MULTI_STD; // this checking must go first else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "QBIRD_MULTI_STH")) nSensor = QBIRD_MULTI_STH; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "QBIRD_MULTI")) nSensor = QBIRD_MULTI; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "WVIEW")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "WVIEW1_PAN_STD") || STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "WVIEW_PAN_STD")) nSensor = WVIEW_PAN_STD; // this checking must go first else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "WVIEW1_PAN") || STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "WVIEW_PAN")) nSensor = WVIEW_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "WVIEW_MULTI_STD")) nSensor = WVIEW_MULTI_STD; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "WVIEW_MULTI")) nSensor = WVIEW_MULTI; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GEOEYE")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GEOEYE_PAN_STD")) nSensor = GEOEYE_PAN_STD; // this checking must go first else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GEOEYE_PAN")) nSensor = GEOEYE_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GEOEYE_MULTI_STD")) nSensor = GEOEYE_MULTI_STD; // this checking must go first else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GEOEYE_MULTI")) nSensor = GEOEYE_MULTI; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "FORMOSAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "FORMOSAT_PAN_L2")) nSensor = FORMOSAT_PAN_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "FORMOSAT_MULTIL2")) nSensor = FORMOSAT_MULTIL2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "FORMOSAT_PAN")) nSensor = FORMOSAT_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "FORMOSAT_MULTI")) nSensor = FORMOSAT_MULTI; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "FORMOSAT5_PAN")) nSensor = FORMOSAT5_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "FORMOSAT5_MS")) nSensor = FORMOSAT5_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT5_PAN_2_5")) nSensor = SPOT5_PAN_2_5; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT5_PAN_5")) nSensor = SPOT5_PAN_5; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT5_HRS")) nSensor = SPOT5_HRS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT5_MULTI")) nSensor = SPOT5_MULTI; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT1_PAN")) nSensor = SPOT1_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT1_MS")) nSensor = SPOT1_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT2_PAN")) nSensor = SPOT2_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT2_MS")) nSensor = SPOT2_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT3_PAN")) nSensor = SPOT3_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT3_MS")) nSensor = SPOT3_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT4_PAN")) nSensor = SPOT4_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT4_MS")) nSensor = SPOT4_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT6_PAN")) nSensor = SPOT6_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT6_MS")) nSensor = SPOT6_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT6_PSH")) nSensor = SPOT6_PSH; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT7_PAN")) nSensor = SPOT7_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT7_MS")) nSensor = SPOT7_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SPOT7_PSH")) nSensor = SPOT7_PSH; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MERIS")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MERIS_FR")) nSensor = MERIS_FR; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MERIS_RR")) nSensor = MERIS_RR; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MERIS_LR")) nSensor = MERIS_LR; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ASAR")) nSensor = ASAR; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "EROS")) nSensor = EROS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MODIS")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MODIS_1000")) nSensor = MODIS_1000; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MODIS_500")) nSensor = MODIS_500; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MODIS_250")) nSensor = MODIS_250; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_HRC_L2")) nSensor = CBERS_HRC_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_HRC")) nSensor = CBERS_HRC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_CCD_L2")) nSensor = CBERS_CCD_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_CCD")) nSensor = CBERS_CCD; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_IRM_80_L2")) nSensor = CBERS_IRM_80_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_IRM_80")) nSensor = CBERS_IRM_80; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_IRM_160_L2")) nSensor = CBERS_IRM_160_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_IRM_160")) nSensor = CBERS_IRM_160; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_WFI_L2")) nSensor = CBERS_WFI_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS_WFI")) nSensor = CBERS_WFI; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS4_PAN_1")) nSensor = CBERS4_PAN_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS4_MS_1")) nSensor = CBERS4_MS_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS4_PAN_2")) nSensor = CBERS4_PAN_2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS4_MS_2")) nSensor = CBERS4_MS_2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS4_THM_1")) nSensor = CBERS4_THM_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CBERS4_THM_2")) nSensor = CBERS4_THM_2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CARTOSAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CARTOSAT1_L1")) nSensor = CARTOSAT1_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "CARTOSAT1_L2")) nSensor = CARTOSAT1_L2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DMC")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DMC_1R")) nSensor = DMC_1R; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DMC_1T")) nSensor = DMC_1T; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALOS")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALOS_PRISM_L1")) nSensor = ALOS_PRISM_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALOS_PRISM_L2")) nSensor = ALOS_PRISM_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALOS_AVNIR_L1")) nSensor = ALOS_AVNIR_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALOS_AVNIR_L2")) nSensor = ALOS_AVNIR_L2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PALSAR")) nSensor = PALSAR; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT2_PAN")) nSensor = KOMPSAT2_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT2_MULTI")) nSensor = KOMPSAT2_MULTI; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT3_PAN")) nSensor = KOMPSAT3_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT3_PSH")) nSensor = KOMPSAT3_PSH; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT3_MS")) nSensor = KOMPSAT3_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT3A_PAN")) nSensor = KOMPSAT3A_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT3A_PSH")) nSensor = KOMPSAT3A_PSH; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KOMPSAT3A_MS")) nSensor = KOMPSAT3A_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TERRASAR")) nSensor = TERRASAR; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "RAPIDEYE")) nSensor = RAPIDEYE_L1B; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "RESOURCESAT")) nSensor = RESOURCESAT; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "THEOS")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "THEOS_PAN_L1")) nSensor = THEOS_PAN_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "THEOS_PAN_L2")) nSensor = THEOS_PAN_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "THEOS_MS_L1")) nSensor = THEOS_MS_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "THEOS_MS_L2")) nSensor = THEOS_MS_L2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GOSAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GOSAT_500_L1")) nSensor = GOSAT_500_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GOSAT_500_L2")) nSensor = GOSAT_500_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GOSAT_1500_L1")) nSensor = GOSAT_1500_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GOSAT_1500_L2")) nSensor = GOSAT_1500_L2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HJ")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HJ_CCD_1A") || STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HJ1A")) nSensor = HJ_CCD_1A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HJ_CC" /* "HJ_CCD_1B" */) || STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HJ1B")) nSensor = HJ_CCD_1B; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HJ1C")) nSensor = HJ1C; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "RASAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "RASAT_PAN")) nSensor = RASAT_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "RASAT_MS")) nSensor = RASAT_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PLEIADES")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PLEIADES_PAN_L1")) nSensor = PLEIADES_PAN_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PLEIADES_MS_L1")) nSensor = PLEIADES_MS_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PLEIADES_PAN_L2")) nSensor = PLEIADES_PAN_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PLEIADES_MS_L2")) nSensor = PLEIADES_MS_L2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TH01")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TH01_DGP")) nSensor = TH01_DGP; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TH01_GFB")) nSensor = TH01_GFB; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TH01_SXZ")) nSensor = TH01_SXZ; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY3_NAD")) nSensor = ZY3_NAD; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY3_FWD")) nSensor = ZY3_FWD; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY3_BWD")) nSensor = ZY3_BWD; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY3_MUX")) nSensor = ZY3_MUX; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY3_TLC")) nSensor = ZY3_TLC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY1_02C_HRC")) nSensor = ZY1_02C_HRC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY1_02C_PMS_PAN")) nSensor = ZY1_02C_PMS_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ZY1_02C_PMS_MS")) nSensor = ZY1_02C_PMS_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GK2")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GK2_PAN")) nSensor = GK2_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GK2_MS")) nSensor = GK2_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MRC")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MRC_RED")) nSensor = MRC_RED; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MRC_GRN")) nSensor = MRC_GRN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MRC_BLU")) nSensor = MRC_BLU; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MRC_NIR")) nSensor = MRC_NIR; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HRC")) nSensor = HRC; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF1_PMS_PAN")) nSensor = GF1_PMS_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF2_PMS_PAN")) nSensor = GF2_PMS_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF1_PMS_MS")) nSensor = GF1_PMS_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF1_WFV")) nSensor = GF1_WFV; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF2_PMS_MS")) nSensor = GF2_PMS_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF4_PMS_MS")) nSensor = GF4_PMS_MS; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF4_PMI_Thermal")) nSensor = GF4_PMI_Thermal; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF6_PMS_PAN")) nSensor = GF6_PMS_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GF6_PMS_MS")) nSensor = GF6_PMS_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SJ9")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SJ9_PAN")) nSensor = SJ9_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SJ9_MUX")) nSensor = SJ9_MUX; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SJ9_PMS_PAN")) nSensor = SJ9_PMS_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SJ9_PMS_MS")) nSensor = SJ9_PMS_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "YG2_1")) nSensor = YG2_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "YG8_1")) nSensor = YG8_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "YG14_1")) nSensor = YG14_1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "UAVSAR")) nSensor = UAVSAR; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SSOT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SSOT_PAN_L1")) nSensor = SSOT_PAN_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SSOT_MS_L1")) nSensor = SSOT_MS_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SSOT_PAN_L2")) nSensor = SSOT_PAN_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SSOT_MS_L2")) nSensor = SSOT_MS_L2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALSAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALSAT2_PAN_1A")) nSensor = ALSAT2_PAN_1A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALSAT2_MS_1A")) nSensor = ALSAT2_MS_1A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALSAT2_PAN_2A")) nSensor = ALSAT2_PAN_2A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "ALSAT2_MS_2A")) nSensor = ALSAT2_MS_2A; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DUBAISAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DUBAISAT2_PAN")) nSensor = DUBAISAT2_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DUBAISAT2_MS")) nSensor = DUBAISAT2_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KAZEOSAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KAZEOSAT1_PAN_1A")) nSensor = KAZEOSAT1_PAN_1A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KAZEOSAT1_MS_1A")) nSensor = KAZEOSAT1_MS_1A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KAZEOSAT1_PAN_2A")) nSensor = KAZEOSAT1_PAN_2A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KAZEOSAT1_MS_2A")) nSensor = KAZEOSAT1_MS_2A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "KAZEOSAT2_MS_1G")) nSensor = KAZEOSAT2_MS_1G; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DEIMOS")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DEIMOS1_MS_1R")) nSensor = DEIMOS1_MS_1R; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DEIMOS2_PAN_1B")) nSensor = DEIMOS2_PAN_1B; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DEIMOS2_MS_1B")) nSensor = DEIMOS2_MS_1B; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "DEIMOS2_PSH_1B")) nSensor = DEIMOS2_PSH_1B; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TRIPLESAT")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TRIPLESAT_PAN")) nSensor = TRIPLESAT_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "TRIPLESAT_MS")) nSensor = TRIPLESAT_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PER_")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PER_PAN_2A")) nSensor = PER_PAN_2A; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "PER_MS_2A")) nSensor = PER_MS_2A; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "JL")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "JL101A_PAN")) nSensor = JL101A_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "JL101A_MS")) nSensor = JL101A_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SV")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SV1_PAN_L1")) nSensor = SV1_PAN_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SV1_MS_L1")) nSensor = SV1_MS_L1; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SV1_PAN_L2")) nSensor = SV1_PAN_L2; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "SV1_MS_L2")) nSensor = SV1_MS_L2; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "GOKTURK1")) { if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "Gokturk1_PAN")) nSensor = GOKTURK1_PAN; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "Gokturk1_MS")) nSensor = GOKTURK1_MS; } else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "HI_RES")) nSensor = HI_RES; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "MED_RES")) nSensor = MED_RES; else if (STARTS_WITH_CI(OrbitPtr->SatelliteSensor.c_str(), "NEW")) nSensor = NEW; else { return ThrowPCIDSKException(0, "Invalid Sensor %s", OrbitPtr->SatelliteSensor.c_str()); } return (nSensor); } /** * Get the model of a sensor * @param nSensor the sensor * @return the model */ int CPCIDSKToutinModelSegment::GetModel( int nSensor ) { int nModel = -999; switch (nSensor) { case PLA_1: case PLA_2: case PLA_3: case PLA_4: case MLA_1: case MLA_2: case MLA_3: case MLA_4: case SPOT1_PAN: case SPOT1_MS: case SPOT2_PAN: case SPOT2_MS: case SPOT3_PAN: case SPOT3_MS: case SPOT4_PAN: case SPOT4_MS: case NEW: nModel = SRITModele; break; case ASTER: case CBERS_CCD: case CBERS_IRM_80: case CBERS_IRM_160: case CBERS_WFI: case IRS_1: case LISS_AWF: case LISS_1: case LISS_2: case LISS_3: case LISS_L3: case LISS_L4: case LISS_P3: case LISS_W3: case LISS_M3: case EOC: case SPOT5_PAN_5: case SPOT5_HRS: case SPOT5_MULTI: case MERIS_FR: case MERIS_RR: case MERIS_LR: case MODIS_1000: case MODIS_500: case MODIS_250: case ALOS_AVNIR_L1: case ALOS_AVNIR_L2: case RAPIDEYE_L1B: case THEOS_PAN_L1: case THEOS_MS_L1: case GOSAT_500_L1: case GOSAT_1500_L1: case HJ_CCD_1A: case RASAT_PAN: case RASAT_MS: case GK2_MS: case GF1_WFV: case YG8_1: case DEIMOS1_MS_1R: case MED_RES: case CBERS4_PAN_1: case CBERS4_MS_1: case CBERS4_THM_1: case SV1_PAN_L1: case SV1_MS_L1: nModel = SRITModele1A; break; case MSS: case TM: case ETM: case LISS_P3_L2: case LISS_L3_L2: case LISS_W3_L2: case LISS_L4_L2: case LISS_AWF_L2: case CBERS_IRM_80_L2: case CBERS_IRM_160_L2: case CBERS_WFI_L2: case CBERS_CCD_L2: case CBERS_HRC_L2: case DMC_1R: case DMC_1T: case ALOS_PRISM_L2: case THEOS_PAN_L2: case THEOS_MS_L2: case GOSAT_500_L2: case GOSAT_1500_L2: case HJ_CCD_1B: case PLEIADES_PAN_L2: case PLEIADES_MS_L2: case SSOT_PAN_L2: case SSOT_MS_L2: case ALSAT2_PAN_2A: case ALSAT2_MS_2A: case RESOURCESAT: case CBERS4_PAN_2: case CBERS4_MS_2: case CBERS4_THM_2: case SV1_PAN_L2: case SV1_MS_L2: nModel = SRITModele1B; break; case SAR: case RSAT_FIN: case RSAT_STD: case ERS_1: case ERS_2: case ASAR: case QBIRD_PAN_STD: case QBIRD_MULTI_STD: case WVIEW_PAN_STD: case WVIEW_MULTI_STD: case GEOEYE_PAN_STD: case GEOEYE_MULTI_STD: case IKO_PAN: case IKO_MULTI: case CARTOSAT1_L2: case PALSAR: case FORMOSAT_PAN_L2: case FORMOSAT_MULTIL2: case TERRASAR: case OV3_PAN_GEO: case OV3_MULTI_GEO: case OV5_PAN_GEO: case OV5_MULTI_GEO: case UAVSAR: case HJ1C: nModel = SRITModeleSAR; break; case ORBVIEW_PAN: case ORBVIEW_MULTI: case QBIRD_PAN: case QBIRD_MULTI: case WVIEW_PAN: case WVIEW_MULTI: case GEOEYE_PAN: case GEOEYE_MULTI: case SPOT5_PAN_2_5: case CARTOSAT1_L1: case ALOS_PRISM_L1: case KOMPSAT2_PAN: case KOMPSAT2_MULTI: case KOMPSAT3_PAN: case KOMPSAT3_PSH: case KOMPSAT3_MS: case KOMPSAT3A_PAN: case KOMPSAT3A_PSH: case KOMPSAT3A_MS: case CBERS_HRC: case OV3_PAN_BASIC: case OV3_MULTI_BASIC: case OV5_PAN_BASIC: case OV5_MULTI_BASIC: case PLEIADES_PAN_L1: case PLEIADES_MS_L1: case SPOT6_PAN: case SPOT6_MS: case SPOT6_PSH: case SPOT7_PAN: case SPOT7_MS: case SPOT7_PSH: case TH01_DGP: case TH01_GFB: case TH01_SXZ: case ZY1_02C_HRC: case ZY1_02C_PMS_PAN: case ZY1_02C_PMS_MS: case ZY3_NAD: case ZY3_FWD: case ZY3_BWD: case ZY3_MUX: case ZY3_TLC: case GK2_PAN: case MRC_RED: case MRC_GRN: case MRC_BLU: case MRC_NIR: case GF1_PMS_PAN: case GF1_PMS_MS: case GF2_PMS_PAN: case GF2_PMS_MS: case GF4_PMS_MS: case GF4_PMI_Thermal: case GF6_PMS_PAN: case GF6_PMS_MS: case SJ9_PAN: case SJ9_MUX: case SJ9_PMS_PAN: case SJ9_PMS_MS: case YG2_1: case YG14_1: case SSOT_PAN_L1: case SSOT_MS_L1: case ALSAT2_PAN_1A: case ALSAT2_MS_1A: case DUBAISAT2_PAN: case DUBAISAT2_MS: case KAZEOSAT1_PAN_1A: case KAZEOSAT1_MS_1A: case KAZEOSAT1_PAN_2A: case KAZEOSAT1_MS_2A: case KAZEOSAT2_MS_1G: case DEIMOS2_PAN_1B: case DEIMOS2_MS_1B: case DEIMOS2_PSH_1B: case TRIPLESAT_PAN: case TRIPLESAT_MS: case PER_PAN_2A: case PER_MS_2A: case JL101A_PAN: case JL101A_MS: case HI_RES: case FORMOSAT5_PAN: case FORMOSAT5_MS: case GOKTURK1_PAN: case GOKTURK1_MS: nModel = SRITModele1AHR; break; case EROS: case HRC: case QBIRD_PAN_STH: case QBIRD_MULTI_STH: case FORMOSAT_PAN: case FORMOSAT_MULTI: nModel = SRITModeleEros; break; default: return ThrowPCIDSKException(0, "Invalid sensor type."); break; } return (nModel); }