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#include <OrbitalInfo.h> |
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|
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using namespace std; |
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|
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ClassImp(OrbitalInfoTrkVar); |
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ClassImp(OrbitalInfo); |
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|
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OrbitalInfoTrkVar::OrbitalInfoTrkVar(){ |
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this->Clear(); |
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// Eij = new TMatrixD(3,3); |
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// Sij = new TMatrixD(3,3); |
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} |
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|
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void OrbitalInfoTrkVar::Clear(Option_t *t){ |
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trkseqno = 0; |
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pitch = -1000.; |
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sunangle = -1000; |
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sunmagangle = -1000; |
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cutoff = -1000.; |
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Eij.Zero(); |
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Sij.Zero(); |
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} |
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|
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void OrbitalInfoTrkVar::Delete(Option_t *t){ |
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// if ( Eij ) Eij->Delete(); |
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// if ( Sij ) Sij->Delete(); |
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} |
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|
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OrbitalInfo::OrbitalInfo(){ |
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OrbitalInfoTrk = 0; //ELENA |
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this->Clear(); |
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} |
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|
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OrbitalInfoTrkVar::OrbitalInfoTrkVar(const OrbitalInfoTrkVar &t){ |
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// |
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trkseqno = t.trkseqno; |
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// |
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pitch = t.pitch; |
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cutoff = t.cutoff; |
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sunangle=t.sunangle; |
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sunmagangle=t.sunmagangle; |
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// |
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Eij.ResizeTo(t.Eij); |
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Eij = t.Eij; |
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Sij.ResizeTo(t.Sij); |
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Sij = t.Sij; |
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// |
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}; |
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|
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void OrbitalInfo::Delete(Option_t *t){ //ELENA |
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// |
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// if ( Iij ) Iij->Delete(); |
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if(OrbitalInfoTrk){ |
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OrbitalInfoTrk->Delete(); //ELENA |
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delete OrbitalInfoTrk; //ELENA |
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} |
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// |
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}; //ELENA |
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|
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void OrbitalInfo::Set(){//ELENA |
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if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA} |
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// if ( !Iij ) Iij = new TMatrixD(3,3); |
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}//ELENA |
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//-------------------------------------- |
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// |
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// |
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//-------------------------------------- |
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void OrbitalInfo::SetTrackArray(TClonesArray *track){//ELENA |
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// if(track && strcmp(track->GetClass()->GetName(),"OrbitalInfoTrkVar")==0){ |
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if(OrbitalInfoTrk)OrbitalInfoTrk->Clear("C"); |
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OrbitalInfoTrk = track; |
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// } |
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} |
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|
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OrbitalInfoTrkVar *OrbitalInfo::GetOrbitalInfoTrkVar(Int_t itrk){ |
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// |
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if(itrk >= ntrk()){ |
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printf(" OrbitalInfo ERROR: track related variables set %i does not exists! \n",itrk); |
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printf(" stored track related variables = %i \n",ntrk()); |
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return(NULL); |
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} |
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// |
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if(!OrbitalInfoTrk)return 0; //ELENA |
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TClonesArray &t = *(OrbitalInfoTrk); |
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OrbitalInfoTrkVar *orbtrack = (OrbitalInfoTrkVar*)t[itrk]; |
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return orbtrack; |
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} |
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/** |
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* Retrieves the tof track matching the seqno-th tracker stored track. |
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* |
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*/ |
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OrbitalInfoTrkVar *OrbitalInfo::GetOrbitalInfoStoredTrack(int seqno){ |
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|
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if( ntrk()==0 ){ |
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printf("OrbitalInfo::GetOrbitalInfoStoredTrack(int) : requested tracker SeqNo %i but no OrbitalInforimeter tracks are stored\n",seqno); |
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return NULL; |
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}; |
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|
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OrbitalInfoTrkVar *c = 0; |
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Int_t it_tof=0; |
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|
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do { |
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c = GetOrbitalInfoTrkVar(it_tof); |
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it_tof++; |
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} while( c && seqno != c->trkseqno && it_tof < ntrk()); |
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|
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if(!c || seqno != c->trkseqno){ |
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c = 0; |
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if(seqno!=-1 ) printf("OrbitalInfo::GetOrbitalInfoStoredTrack(int) : requested tracker SeqNo %i does not match OrbitalInfo stored tracks\n",seqno); |
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}; |
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return c; |
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|
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} |
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|
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void OrbitalInfo::Clear(Option_t *t){ |
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// |
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if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete(); |
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// |
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absTime = 0; |
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OBT = 0; |
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pkt_num = 0; |
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|
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lon = -1000.; |
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lat = -1000.; |
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alt = -1000.; |
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V.SetXYZ(-1000.,-1000.,-1000.); |
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|
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Bnorth = -1000.; |
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Beast = -1000.; |
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Bdown = -1000.; |
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Babs = -1000.; |
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M = -1000; |
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BB0 = -1000.; |
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L = -1000.; |
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|
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londip = -1000.; |
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latdip = -1000.; |
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|
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// std::fill_n(cutoff, 20, 0.); |
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// std::fill_n(cutoff, 2, 0.); |
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cutoffsvl = 0.; |
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|
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// Quaternions |
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q0 = -1000.; |
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q1 = -1000.; |
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q2 = -1000.; |
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q3 = -1000.; |
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|
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// Euler angles (nadir reference frame) |
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theta = -1000.; |
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phi = -1000.; |
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etha = -1000.; |
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|
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Iij.Zero(); |
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|
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mode = 0; |
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qkind = -1000; |
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errq = -1000; |
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azim = -1000; |
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rtqual =-1000; |
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// std::fill_n(goodAttitude, 5, 0); |
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} |
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|
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/** |
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* Fills a struct cOrbitalInfo with values from a OrbitalInfo object (to put data into a F77 common). |
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*/ |
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void OrbitalInfo::GetLevel2Struct(cOrbitalInfo *l2) const{ |
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l2->abstime = absTime; |
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l2->obt = OBT; |
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l2->pkt_num = pkt_num; |
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|
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l2->lon = lon; |
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l2->lat = lat; |
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l2->alt = alt; |
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l2->V = V; |
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|
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l2->Bnorth = Bnorth; |
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l2->Beast = Beast; |
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l2->Bdown = Bdown; |
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l2->Babs = Babs; |
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l2->M = M; |
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l2->BB0 = BB0; |
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l2->L = L; |
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|
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l2->londip = londip; |
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l2->latdip = latdip; |
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|
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l2->cutoffsvl = cutoffsvl; |
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// memcpy(l2->cutoffsvl, cutoffsvl, sizeof(cutoffsvl)); |
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|
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// Quaternions |
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l2->q0 = q0; |
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l2->q1 = q1; |
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l2->q2 = q2; |
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l2->q3 = q3; |
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|
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// Euler angles (nadir reference frame) |
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l2->theta = theta; |
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l2->phi = phi; |
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l2->etha = etha; |
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|
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l2->mode = mode; |
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l2->qkind = qkind; |
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l2->errq = errq; |
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l2->azim = azim; |
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l2->rtqual=rtqual; |
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|
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l2->Iij=Iij; |
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|
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// memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude)); |
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} |
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|
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void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){ |
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absTime = l2->abstime; |
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OBT = l2->obt; |
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pkt_num = l2->pkt_num; |
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|
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lon = l2->lon; |
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lat = l2->lat; |
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alt = l2->alt; |
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V = l2->V; |
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|
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Bnorth = l2->Bnorth; |
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Beast = l2->Beast; |
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Bdown = l2->Bdown; |
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Babs = l2->Babs; |
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M = l2->M; |
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BB0 = l2->BB0; |
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L = l2->L; |
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|
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londip = l2->londip; |
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latdip = l2->latdip; |
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|
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// memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff)); |
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l2->cutoffsvl = cutoffsvl; |
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|
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// Quaternions |
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q0 = l2->q0; |
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q1 = l2->q1; |
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q2 = l2->q2; |
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q3 = l2->q3; |
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|
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// Euler angles (nadir reference frame) |
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theta = l2->theta; |
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phi = l2->phi; |
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etha = l2->etha; |
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|
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mode = l2->mode; |
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qkind = l2->qkind; |
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errq = l2->errq; |
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azim = l2->azim; |
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rtqual=l2->rtqual; |
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|
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Iij=l2->Iij; |
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|
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// memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude)); |
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} |
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