OrbitalInfo/src/OrbitalInfo.cpp

#include <OrbitalInfo.h>

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));
}

1	#include <OrbitalInfo.h>
2
3	using namespace std;
4
5	ClassImp(OrbitalInfoTrkVar);
6	ClassImp(OrbitalInfo);
7
8	OrbitalInfoTrkVar::OrbitalInfoTrkVar(){
9	this->Clear();
10	}
11
12	void OrbitalInfoTrkVar::Clear(Option_t *t){
13	trkseqno = 0;
14	pitch = -1000.;
15	}
16
17
18	OrbitalInfo::OrbitalInfo(){
19	OrbitalInfoTrk = 0; //ELENA
20	this->Clear();
21	}
22
23	void OrbitalInfo::Delete(Option_t *t){ //ELENA
24	//
25	if(OrbitalInfoTrk){
26	OrbitalInfoTrk->Delete(); //ELENA
27	delete OrbitalInfoTrk; //ELENA
28	}
29	//
30	}; //ELENA
31
32	void OrbitalInfo::Set(){//ELENA
33	if ( !OrbitalInfoTrk ) OrbitalInfoTrk = new TClonesArray("OrbitalInfoTrkVar",2); //ELENA
34	}//ELENA
35
36
37	void OrbitalInfo::Clear(Option_t *t){
38	//
39	if ( OrbitalInfoTrk ) OrbitalInfoTrk->Delete();
40	//
41	absTime = 0;
42	OBT = 0;
43	pkt_num = 0;
44
45	lon = -1000.;
46	lat = -1000.;
47	alt = -1000.;
48
49	Bnorth = -1000.;
50	Beast = -1000.;
51	Bdown = -1000.;
52	Babs = -1000.;
53	BB0 = -1000.;
54	L = -1000.;
55
56	londip = -1000.;
57	latdip = -1000.;
58	altdip = -1000.;
59
60	loncgm = -1000.;
61	latcgm = -1000.;
62	altcgm = -1000.;
63
64	loncbm = -1000.;
65	latcbm = -1000.;
66	altcbm = -1000.;
67
68	std::fill_n(cutoff, 20, 0.);
69
70	// Quaternions
71	q0 = -1000.;
72	q1 = -1000.;
73	q2 = -1000.;
74	q3 = -1000.;
75
76	// Euler angles (nadir reference frame)
77	theta = -1000.;
78	phi = -1000.;
79	etha = -1000.;
80
81	// Euler angles (local field reference frame)
82	// thetamag = -1000.;
83	// phimag = -1000.;
84	// ethamag = -1000.;
85
86	pamzenitangle = -1000.;
87	pamBangle = -1000.;
88
89
90	mode = 0;
91	// std::fill_n(goodAttitude, 5, 0);
92	}
93
94	/**
95	* Fills a struct cOrbitalInfo with values from a OrbitalInfo object (to put data into a F77 common).
96	*/
97	void OrbitalInfo::GetLevel2Struct(cOrbitalInfo *l2) const{
98	l2->abstime = absTime;
99	l2->obt = OBT;
100	l2->pkt_num = pkt_num;
101
102	l2->lon = lon;
103	l2->lat = lat;
104	l2->alt = alt;
105
106	l2->Bnorth = Bnorth;
107	l2->Beast = Beast;
108	l2->Bdown = Bdown;
109	l2->Babs = Babs;
110	l2->BB0 = BB0;
111	l2->L = L;
112
113	l2->londip = londip;
114	l2->latdip = latdip;
115	l2->altdip = altdip;
116
117	l2->loncgm = loncgm;
118	l2->latcgm = latcgm;
119	l2->altcgm = altcgm;
120
121	l2->loncbm = loncbm;
122	l2->latcbm = latcbm;
123	l2->altcbm = altcbm;
124
125	memcpy(l2->cutoff, cutoff, sizeof(cutoff));
126
127	// Quaternions
128	l2->q0 = q0;
129	l2->q1 = q1;
130	l2->q2 = q2;
131	l2->q3 = q3;
132
133	// Euler angles (nadir reference frame)
134	l2->theta = theta;
135	l2->phi = phi;
136	l2->etha = etha;
137
138	l2->mode = mode;
139	// Euler angles (local field reference frame)
140	// l2->thetamag = thetamag;
141	// l2->phimag = phimag;
142	// l2->ethamag = ethamag;
143
144	// memcpy(l2->goodAttitude, goodAttitude, sizeof(goodAttitude));
145	}
146
147	void OrbitalInfo::SetFromLevel2Struct(cOrbitalInfo *l2){
148	absTime = l2->abstime;
149	OBT = l2->obt;
150	pkt_num = l2->pkt_num;
151
152	lon = l2->lon;
153	lat = l2->lat;
154	alt = l2->alt;
155
156	l2->Bnorth = Bnorth;
157	l2->Beast = Beast;
158	l2->Bdown = Bdown;
159	l2->Babs = Babs;
160	BB0 = l2->BB0;
161	L = l2->L;
162
163	londip = l2->londip;
164	latdip = l2->latdip;
165	altdip = l2->altdip;
166
167	loncgm = l2->loncgm;
168	latcgm = l2->latcgm;
169	altcgm = l2->altcgm;
170
171	loncbm = l2->loncbm;
172	latcbm = l2->latcbm;
173	altcbm = l2->altcbm;
174
175	memcpy(cutoff, l2->cutoff, sizeof(l2->cutoff));
176
177	// Quaternions
178	q0 = l2->q0;
179	q1 = l2->q1;
180	q2 = l2->q2;
181	q3 = l2->q3;
182
183	// Euler angles (nadir reference frame)
184	theta = l2->theta;
185	phi = l2->phi;
186	etha = l2->etha;
187
188	mode = l2->mode;
189	// Euler angles (local field reference frame)
190	// thetamag = l2->thetamag;
191	// phimag = l2->phimag;
192	// ethamag = l2->ethamag;
193
194	// memcpy(goodAttitude, l2->goodAttitude, sizeof(l2->goodAttitude));
195	}
196