#include using namespace std; ClassImp(OrbitalInfoTrkVar); ClassImp(OrbitalInfo); OrbitalInfoTrkVar::OrbitalInfoTrkVar(){ this->Clear(); // Eij = new TMatrixD(3,3); // Sij = new TMatrixD(3,3); } void OrbitalInfoTrkVar::Clear(Option_t *t){ trkseqno = 0; pitch = -1000.; sunangle = -1000; sunmagangle = -1000; cutoff = -1000.; Eij.Zero(); Sij.Zero(); } void OrbitalInfoTrkVar::Delete(Option_t *t){ // if ( Eij ) Eij->Delete(); // if ( Sij ) Sij->Delete(); } OrbitalInfo::OrbitalInfo(){ OrbitalInfoTrk = 0; //ELENA this->Clear(); } OrbitalInfoTrkVar::OrbitalInfoTrkVar(const OrbitalInfoTrkVar &t){ // trkseqno = t.trkseqno; // pitch = t.pitch; cutoff = t.cutoff; sunangle=t.sunangle; sunmagangle=t.sunmagangle; // Eij.ResizeTo(t.Eij); Eij = t.Eij; Sij.ResizeTo(t.Sij); Sij = t.Sij; // }; void OrbitalInfo::Delete(Option_t *t){ //ELENA // // if ( Iij ) Iij->Delete(); if(OrbitalInfoTrk){ OrbitalInfoTrk->Delete(); //ELENA delete OrbitalInfoTrk; //ELENA } // }; //ELENA void OrbitalInfo::Set(){//ELENA if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA} // if ( !Iij ) Iij = new TMatrixD(3,3); }//ELENA OrbitalInfoTrkVar *OrbitalInfo::GetOrbitalInfoTrkVar(Int_t itrk){ // if(itrk >= ntrk()){ printf(" OrbitalInfo ERROR: track related variables set %i does not exists! \n",itrk); printf(" stored track related variables = %i \n",ntrk()); return(NULL); } // if(!OrbitalInfoTrk)return 0; //ELENA TClonesArray &t = *(OrbitalInfoTrk); OrbitalInfoTrkVar *orbtrack = (OrbitalInfoTrkVar*)t[itrk]; return orbtrack; } void OrbitalInfo::Clear(Option_t *t){ // if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete(); // absTime = 0; OBT = 0; pkt_num = 0; lon = -1000.; lat = -1000.; alt = -1000.; V.SetXYZ(-1000.,-1000.,-1000.); Bnorth = -1000.; Beast = -1000.; Bdown = -1000.; Babs = -1000.; M = -1000; BB0 = -1000.; L = -1000.; londip = -1000.; latdip = -1000.; // std::fill_n(cutoff, 20, 0.); // std::fill_n(cutoff, 2, 0.); cutoffsvl = 0.; // Quaternions q0 = -1000.; q1 = -1000.; q2 = -1000.; q3 = -1000.; // Euler angles (nadir reference frame) theta = -1000.; phi = -1000.; etha = -1000.; Iij.Zero(); mode = 0; qkind = -1000; errq = -1000; azim = -1000; // std::fill_n(goodAttitude, 5, 0); } /** * Fills a struct cOrbitalInfo with values from a OrbitalInfo object (to put data into a F77 common). */ void OrbitalInfo::GetLevel2Struct(cOrbitalInfo *l2) const{ l2->abstime = absTime; l2->obt = OBT; l2->pkt_num = pkt_num; l2->lon = lon; l2->lat = lat; l2->alt = alt; l2->V = V; l2->Bnorth = Bnorth; l2->Beast = Beast; l2->Bdown = Bdown; l2->Babs = Babs; l2->M = M; l2->BB0 = BB0; l2->L = L; l2->londip = londip; l2->latdip = latdip; l2->cutoffsvl = cutoffsvl; // memcpy(l2->cutoffsvl, cutoffsvl, sizeof(cutoffsvl)); // Quaternions l2->q0 = q0; l2->q1 = q1; l2->q2 = q2; l2->q3 = q3; // Euler angles (nadir reference frame) l2->theta = theta; l2->phi = phi; l2->etha = etha; l2->mode = mode; l2->qkind = qkind; l2->errq = errq; l2->azim = azim; // memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude)); } void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){ absTime = l2->abstime; OBT = l2->obt; pkt_num = l2->pkt_num; lon = l2->lon; lat = l2->lat; alt = l2->alt; V = l2->V; l2->Bnorth = Bnorth; l2->Beast = Beast; l2->Bdown = Bdown; l2->Babs = Babs; M = l2->M; BB0 = l2->BB0; L = l2->L; londip = l2->londip; latdip = l2->latdip; // memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff)); l2->cutoffsvl = cutoffsvl; // Quaternions q0 = l2->q0; q1 = l2->q1; q2 = l2->q2; q3 = l2->q3; // Euler angles (nadir reference frame) theta = l2->theta; phi = l2->phi; etha = l2->etha; mode = l2->mode; qkind = l2->qkind; errq = l2->errq; azim = l2->azim; // memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude)); }