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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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} |
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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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} |
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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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void OrbitalInfo::Delete(Option_t *t){ //ELENA |
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// |
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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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}//ELENA |
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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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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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|
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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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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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altdip = -1000.; |
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|
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loncgm = -1000.; |
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latcgm = -1000.; |
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altcgm = -1000.; |
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|
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loncbm = -1000.; |
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latcbm = -1000.; |
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altcbm = -1000.; |
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|
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std::fill_n(cutoff, 20, 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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// Euler angles (local field reference frame) |
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// thetamag = -1000.; |
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// phimag = -1000.; |
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// ethamag = -1000.; |
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|
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pamzenitangle = -1000.; |
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pamBangle = -1000.; |
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|
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|
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mode = 0; |
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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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|
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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->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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l2->altdip = altdip; |
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|
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l2->loncgm = loncgm; |
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l2->latcgm = latcgm; |
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l2->altcgm = altcgm; |
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|
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l2->loncbm = loncbm; |
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l2->latcbm = latcbm; |
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l2->altcbm = altcbm; |
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|
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memcpy(l2->cutoff, cutoff, sizeof(cutoff)); |
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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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// Euler angles (local field reference frame) |
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// l2->thetamag = thetamag; |
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// l2->phimag = phimag; |
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// l2->ethamag = ethamag; |
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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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|
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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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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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altdip = l2->altdip; |
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|
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loncgm = l2->loncgm; |
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latcgm = l2->latcgm; |
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altcgm = l2->altcgm; |
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|
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loncbm = l2->loncbm; |
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latcbm = l2->latcbm; |
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altcbm = l2->altcbm; |
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|
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memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff)); |
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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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// Euler angles (local field reference frame) |
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// thetamag = l2->thetamag; |
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// phimag = l2->phimag; |
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// ethamag = l2->ethamag; |
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|
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// memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude)); |
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} |
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