#include using namespace std; ClassImp(OrbitalInfoTrkVar); ClassImp(OrbitalInfo); OrbitalInfoTrkVar::OrbitalInfoTrkVar(){ this->Clear(); } void OrbitalInfoTrkVar::Clear(Option_t *t){ trkseqno = 0; pitch = -1000.; } OrbitalInfo::OrbitalInfo(){ OrbitalInfoTrk = 0; //ELENA this->Clear(); } void OrbitalInfo::Delete(Option_t *t){ //ELENA // if(OrbitalInfoTrk){ OrbitalInfoTrk->Delete(); //ELENA delete OrbitalInfoTrk; //ELENA } // }; //ELENA void OrbitalInfo::Set(){//ELENA if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA }//ELENA void OrbitalInfo::Clear(Option_t *t){ // if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete(); // absTime = 0; OBT = 0; pkt_num = 0; lon = -1000.; lat = -1000.; alt = -1000.; Bnorth = -1000.; Beast = -1000.; Bdown = -1000.; Babs = -1000.; BB0 = -1000.; L = -1000.; londip = -1000.; latdip = -1000.; altdip = -1000.; loncgm = -1000.; latcgm = -1000.; altcgm = -1000.; loncbm = -1000.; latcbm = -1000.; altcbm = -1000.; std::fill_n(cutoff, 20, 0.); // Quaternions q0 = -1000.; q1 = -1000.; q2 = -1000.; q3 = -1000.; // Euler angles (nadir reference frame) theta = -1000.; phi = -1000.; etha = -1000.; // Euler angles (local field reference frame) // thetamag = -1000.; // phimag = -1000.; // ethamag = -1000.; pamzenitangle = -1000.; pamBangle = -1000.; mode = 0; // 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->Bnorth = Bnorth; l2->Beast = Beast; l2->Bdown = Bdown; l2->Babs = Babs; l2->BB0 = BB0; l2->L = L; l2->londip = londip; l2->latdip = latdip; l2->altdip = altdip; l2->loncgm = loncgm; l2->latcgm = latcgm; l2->altcgm = altcgm; l2->loncbm = loncbm; l2->latcbm = latcbm; l2->altcbm = altcbm; memcpy(l2->cutoff, cutoff, sizeof(cutoff)); // 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; // Euler angles (local field reference frame) // l2->thetamag = thetamag; // l2->phimag = phimag; // l2->ethamag = ethamag; // 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; l2->Bnorth = Bnorth; l2->Beast = Beast; l2->Bdown = Bdown; l2->Babs = Babs; BB0 = l2->BB0; L = l2->L; londip = l2->londip; latdip = l2->latdip; altdip = l2->altdip; loncgm = l2->loncgm; latcgm = l2->latcgm; altcgm = l2->altcgm; loncbm = l2->loncbm; latcbm = l2->latcbm; altcbm = l2->altcbm; memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff)); // 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; // Euler angles (local field reference frame) // thetamag = l2->thetamag; // phimag = l2->phimag; // ethamag = l2->ethamag; // memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude)); }