--- DarthVader/OrbitalInfo/src/OrbitalInfo.cpp 2006/06/14 09:52:54 1.2 +++ DarthVader/OrbitalInfo/src/OrbitalInfo.cpp 2014/10/15 12:06:49 1.17 @@ -1,11 +1,251 @@ #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(){ - absTime = 0ULL; - OBT = 0ULL; - pkt_num = 0ULL; + 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 +//-------------------------------------- +// +// +//-------------------------------------- +void OrbitalInfo::SetTrackArray(TClonesArray *track){//ELENA +// if(track && strcmp(track->GetClass()->GetName(),"OrbitalInfoTrkVar")==0){ + if(OrbitalInfoTrk)OrbitalInfoTrk->Clear("C"); + OrbitalInfoTrk = track; +// } } +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; +} +/** + * Retrieves the tof track matching the seqno-th tracker stored track. + * + */ +OrbitalInfoTrkVar *OrbitalInfo::GetOrbitalInfoStoredTrack(int seqno){ + + if( ntrk()==0 ){ + printf("OrbitalInfo::GetOrbitalInfoStoredTrack(int) : requested tracker SeqNo %i but no OrbitalInforimeter tracks are stored\n",seqno); + return NULL; + }; + + OrbitalInfoTrkVar *c = 0; + Int_t it_tof=0; + + do { + c = GetOrbitalInfoTrkVar(it_tof); + it_tof++; + } while( c && seqno != c->trkseqno && it_tof < ntrk()); + + if(!c || seqno != c->trkseqno){ + c = 0; + if(seqno!=-1 ) printf("OrbitalInfo::GetOrbitalInfoStoredTrack(int) : requested tracker SeqNo %i does not match OrbitalInfo stored tracks\n",seqno); + }; + return c; + +} + +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)); +} -ClassImp(OrbitalInfo) -