OrbitalInfo/src/OrbitalInfo.cpp

#include <OrbitalInfo.h>

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.;
  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();
}

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.;

  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.);
  //  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.;

  // Euler angles (local field reference frame)
  //  thetamag = -1000.;
  //  phimag = -1000.;
  //  ethamag = -1000.;

  //  pamzenitangle = -1000.;
  //  pamBangle = -1000.;
  Iij.Zero();

  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;

  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;
  // 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));
  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;
  // Euler angles (local field reference frame)
//   thetamag = l2->thetamag;
//   phimag = l2->phimag;
//   ethamag = l2->ethamag;

//   memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
}

1	#include <OrbitalInfo.h>
2
3	using namespace std;
4
5	ClassImp(OrbitalInfoTrkVar);
6	ClassImp(OrbitalInfo);
7
8	OrbitalInfoTrkVar::OrbitalInfoTrkVar(){
9	this->Clear();
10	// Eij = new TMatrixD(3,3);
11	// Sij = new TMatrixD(3,3);
12	}
13
14	void OrbitalInfoTrkVar::Clear(Option_t *t){
15	trkseqno = 0;
16	pitch = -1000.;
17	Eij.Zero();
18	Sij.Zero();
19	}
20
21	void OrbitalInfoTrkVar::Delete(Option_t *t){
22	// if ( Eij ) Eij->Delete();
23	// if ( Sij ) Sij->Delete();
24	}
25
26	OrbitalInfo::OrbitalInfo(){
27	OrbitalInfoTrk = 0; //ELENA
28	this->Clear();
29	}
30
31	void OrbitalInfo::Delete(Option_t *t){ //ELENA
32	//
33	// if ( Iij ) Iij->Delete();
34	if(OrbitalInfoTrk){
35	OrbitalInfoTrk->Delete(); //ELENA
36	delete OrbitalInfoTrk; //ELENA
37	}
38	//
39	}; //ELENA
40
41	void OrbitalInfo::Set(){//ELENA
42	if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA}
43	// if ( !Iij ) Iij = new TMatrixD(3,3);
44	}//ELENA
45
46	OrbitalInfoTrkVar *OrbitalInfo::GetOrbitalInfoTrkVar(Int_t itrk){
47	//
48	if(itrk >= ntrk()){
49	printf(" OrbitalInfo ERROR: track related variables set %i does not exists! \n",itrk);
50	printf(" stored track related variables = %i \n",ntrk());
51	return(NULL);
52	}
53	//
54	if(!OrbitalInfoTrk)return 0; //ELENA
55	TClonesArray &t = *(OrbitalInfoTrk);
56	OrbitalInfoTrkVar orbtrack = (OrbitalInfoTrkVar)t[itrk];
57	return orbtrack;
58	}
59
60	void OrbitalInfo::Clear(Option_t *t){
61	//
62	if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete();
63	//
64	absTime = 0;
65	OBT = 0;
66	pkt_num = 0;
67
68	lon = -1000.;
69	lat = -1000.;
70	alt = -1000.;
71
72	Bnorth = -1000.;
73	Beast = -1000.;
74	Bdown = -1000.;
75	Babs = -1000.;
76	BB0 = -1000.;
77	L = -1000.;
78
79	// londip = -1000.;
80	// latdip = -1000.;
81	// altdip = -1000.;
82
83	// loncgm = -1000.;
84	// latcgm = -1000.;
85	// altcgm = -1000.;
86
87	// loncbm = -1000.;
88	// latcbm = -1000.;
89	// altcbm = -1000.;
90
91	// std::fill_n(cutoff, 20, 0.);
92	// std::fill_n(cutoff, 2, 0.);
93	cutoffsvl = 0.;
94
95	// Quaternions
96	q0 = -1000.;
97	q1 = -1000.;
98	q2 = -1000.;
99	q3 = -1000.;
100
101	// Euler angles (nadir reference frame)
102	theta = -1000.;
103	phi = -1000.;
104	etha = -1000.;
105
106	// Euler angles (local field reference frame)
107	// thetamag = -1000.;
108	// phimag = -1000.;
109	// ethamag = -1000.;
110
111	// pamzenitangle = -1000.;
112	// pamBangle = -1000.;
113	Iij.Zero();
114
115	mode = 0;
116	// std::fill_n(goodAttitude, 5, 0);
117	}
118
119	/**
120	* Fills a struct cOrbitalInfo with values from a OrbitalInfo object (to put data into a F77 common).
121	*/
122	void OrbitalInfo::GetLevel2Struct(cOrbitalInfo *l2) const{
123	l2->abstime = absTime;
124	l2->obt = OBT;
125	l2->pkt_num = pkt_num;
126
127	l2->lon = lon;
128	l2->lat = lat;
129	l2->alt = alt;
130
131	l2->Bnorth = Bnorth;
132	l2->Beast = Beast;
133	l2->Bdown = Bdown;
134	l2->Babs = Babs;
135	l2->BB0 = BB0;
136	l2->L = L;
137
138	// l2->londip = londip;
139	// l2->latdip = latdip;
140	// l2->altdip = altdip;
141
142	// l2->loncgm = loncgm;
143	// l2->latcgm = latcgm;
144	// l2->altcgm = altcgm;
145
146	// l2->loncbm = loncbm;
147	// l2->latcbm = latcbm;
148	// l2->altcbm = altcbm;
149
150	l2->cutoffsvl = cutoffsvl;
151	// memcpy(l2->cutoffsvl, cutoffsvl, sizeof(cutoffsvl));
152
153	// Quaternions
154	l2->q0 = q0;
155	l2->q1 = q1;
156	l2->q2 = q2;
157	l2->q3 = q3;
158
159	// Euler angles (nadir reference frame)
160	l2->theta = theta;
161	l2->phi = phi;
162	l2->etha = etha;
163
164	l2->mode = mode;
165	// Euler angles (local field reference frame)
166	// l2->thetamag = thetamag;
167	// l2->phimag = phimag;
168	// l2->ethamag = ethamag;
169
170	// memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
171	}
172
173	void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){
174	absTime = l2->abstime;
175	OBT = l2->obt;
176	pkt_num = l2->pkt_num;
177
178	lon = l2->lon;
179	lat = l2->lat;
180	alt = l2->alt;
181
182	l2->Bnorth = Bnorth;
183	l2->Beast = Beast;
184	l2->Bdown = Bdown;
185	l2->Babs = Babs;
186	BB0 = l2->BB0;
187	L = l2->L;
188
189	// londip = l2->londip;
190	// latdip = l2->latdip;
191	// altdip = l2->altdip;
192
193	// loncgm = l2->loncgm;
194	// latcgm = l2->latcgm;
195	// altcgm = l2->altcgm;
196
197	// loncbm = l2->loncbm;
198	// latcbm = l2->latcbm;
199	// altcbm = l2->altcbm;
200
201	// memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff));
202	l2->cutoffsvl = cutoffsvl;
203
204	// Quaternions
205	q0 = l2->q0;
206	q1 = l2->q1;
207	q2 = l2->q2;
208	q3 = l2->q3;
209
210	// Euler angles (nadir reference frame)
211	theta = l2->theta;
212	phi = l2->phi;
213	etha = l2->etha;
214
215	mode = l2->mode;
216	// Euler angles (local field reference frame)
217	// thetamag = l2->thetamag;
218	// phimag = l2->phimag;
219	// ethamag = l2->ethamag;
220
221	// memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
222	}
223