/[PAMELA software]/DarthVader/OrbitalInfo/src/InclinationInfo.cpp
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Contents of /DarthVader/OrbitalInfo/src/InclinationInfo.cpp

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Revision 1.4 - (show annotations) (download)
Wed Apr 18 14:06:44 2007 UTC (17 years, 7 months ago) by mocchiut
Branch: MAIN
CVS Tags: v3r04, v3r05, v3r03, v4r00, v3r06
Changes since 1.3: +49 -438 lines
Inclination variables added

1 /***************************************************************************
2 * Copyright (C) 2006 by pamelaprod *
3 * pamelaprod@P1.pamela *
4 * *
5 * This program is free software; you can redistribute it and/or modify *
6 * it under the terms of the GNU General Public License as published by *
7 * the Free Software Foundation; either version 2 of the License, or *
8 * (at your option) any later version. *
9 * *
10 * This program is distributed in the hope that it will be useful, *
11 * but WITHOUT ANY WARRANTY; without even the implied warranty of *
12 * MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the *
13 * GNU General Public License for more details. *
14 * *
15 * You should have received a copy of the GNU General Public License *
16 * along with this program; if not, write to the *
17 * Free Software Foundation, Inc., *
18 * 59 Temple Place - Suite 330, Boston, MA 02111-1307, USA. *
19 ***************************************************************************/
20 #include <InclinationInfo.h>
21 #include <TMath.h>
22 #include <TMatrixD.h>
23
24 using namespace std;
25
26 // InclinationInfoI()::InclinationInfoI() {
27 // // memset(time,0,6*sizeof(double));
28 // // memset(quad,0,6*4*sizeof(double));
29 // };
30
31 void InclinationInfoI::fill(TArrayC* data){
32 short extIndex = 0;
33 short innIndex = 0;
34 long tempData = 0;
35 for (int i = 0; i < 6; i++){
36 extIndex = 20*i;
37 time[i] = (((data->At(extIndex) << 24) & 0xFF000000) +
38 ((data->At(extIndex + 1) << 16) & 0x00FF0000) + ((data->At(extIndex + 2) << 8) & 0x0000FF00) +
39 (data->At(extIndex + 3) & 0x000000FF))/128.0;
40 for (int j = 0; j < 4; j++){
41 innIndex = extIndex + 4*j;
42 tempData = ((data->At(innIndex + 4) << 24) & 0xFF000000) + ((data->At(innIndex + 5) << 16) & 0x00FF0000) + ((data->At(innIndex + 6) << 8) & 0x0000FF00) + (data->At(innIndex + 7) & 0x000000FF);
43 if (data->At(innIndex + 4) >> 8) {
44 quat[i][j] = (~tempData * -1.0)/1073741824.0;
45 } else {
46 quat[i][j] = tempData / 1073741824.0;
47 }
48 }
49 }
50 }
51
52 void InclinationInfoI::clear() {
53 for(UInt_t i = 0; i < 6; i++){
54 time[i]=0;
55 for(UInt_t j = 0; j < 4; j++) quat[i][j]=0;
56 }
57 return ;
58 }
59
60
61 Quaternions::Quaternions()
62 : InclinationInfoI()
63 {
64 }
65
66
67 Quaternions::~Quaternions()
68 {
69 }
70
71 InclinationInfo::InclinationInfo()
72 : TObject()
73 {
74 }
75
76 InclinationInfo::~InclinationInfo()
77 {
78 }
79
80 short int Sign_1(double_t a, Int_t b){
81 if(a>0){b=1;}
82 if(a<0){b=-1;}
83 else{b=0;}
84 return b;
85 }
86
87
88 /******************************************************************************************************************/
89 /******************************************************************************************************************/
90 //********************* ***************************************************************/
91 //********************* COORDINATE SYSTEMS ***************************************************************/
92 //********************* ***************************************************************/
93 //*****************************************************************************************************************/
94 //*****************************************************************************************************************/
95 //
96 // ZISK
97 // +
98 // / \ YOSK ZOSK (Directed by Radius)
99 // | _ _.
100 // | |\ /|
101 // | \ /
102 // | \ /
103 // |.__..__ \ /
104 // Orbit _._.***| **.\/_ XOSK (Directed by velocity)
105 // .* | (X0,Y0,Z0) **--.___|
106 // _** | / *. /
107 // .* | * *
108 // * ..****|***.. / R *
109 // .* | .*.
110 // .* | / *.
111 // * EARTH | / * YISK
112 // * | /_ _ _*_ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _|
113 // * / * /
114 // * / .*
115 // *. / .*
116 // **/*******
117 // /
118 // /
119 // /
120 // /
121 // /
122 // /
123 // |/
124 // *--
125 // XISK
126 //
127 //****************************************************************************************************/
128 //****************************************************************************************************/
129
130
131 void InclinationInfo::TransAngle(Double_t x0, Double_t y0, Double_t z0, Double_t Vx0, Double_t Vy0, Double_t Vz0, Double_t q0, Double_t q1, Double_t q2, Double_t q3){
132
133 double_t a = 360/(2*TMath::Pi());
134
135 TMatrixD Xij(3,3);
136 Xij(0,0) = 1; Xij(0,1) = 0; Xij(0,2) = 0;
137 Xij(1,0) = 0; Xij(1,1) = 0; Xij(1,2) = 1;
138 Xij(2,0) = 0; Xij(2,1) = -1; Xij(2,2) = 0;
139
140 TMatrixD Zij(3,3);
141 Zij(0,0) = 0; Zij(0,1) = 0; Zij(0,2) = -1;
142 Zij(1,0) = -1; Zij(1,1) = 0; Zij(1,2) = 0;
143 Zij(2,0) = 0; Zij(2,1) = 1; Zij(2,2) = 0;
144
145 TMatrixD Pij(3,3);
146 Pij(0,0) = pow(q0,2)+pow(q1,2)-pow(q2,2)-pow(q3,2);
147 Pij(0,1) = /*2*(q1*q2+q0*q3);/*/ 2*(q1*q2-q0*q3);
148 Pij(0,2) = /*2*(q1*q3-q0*q2);/*/ 2*(q1*q3+q0*q2);
149 Pij(1,0) = /*2*(q1*q2-q0*q3);/*/ 2*(q1*q2+q0*q3);
150 Pij(1,1) = pow(q0,2)-pow(q1,2)+pow(q2,2)-pow(q3,2);
151 Pij(1,2) = /*2*(q2*q3+q0*q1);/*/ 2*(q2*q3-q0*q1);
152 Pij(2,0) = /*2*(q1*q3+q0*q2);/*/ 2*(q1*q3-q0*q2);
153 Pij(2,1) = /*2*(q2*q3-q0*q1);/*/ 2*(q2*q3+q0*q1);
154 Pij(2,2) = pow(q0,2)-pow(q1,2)-pow(q2,2)+pow(q3,2);
155
156 TMatrixD Aij(3,3);
157
158 Double_t C1 = y0*Vz0 - z0*Vy0;
159 Double_t C2 = z0*Vx0 - x0*Vz0;
160 Double_t C3 = x0*Vy0 - y0*Vx0;
161 Double_t C = sqrt(pow(C1,2) + pow(C2,2) + pow(C3,2));
162 Double_t V0 = sqrt(pow(Vx0,2)+pow(Vy0,2) + pow(Vz0,2));
163 // Double_t R0 = sqrt(pow(x0,2)+pow(y0,2) + pow(z0,2));
164 Aij(0,0) = /*(C2*z0-C3*y0)/(C*R0);/*/Vx0/V0;
165 Aij(0,1) = C1/C;
166 Aij(0,2) = /*x0/R0;/*/(Vy0*C3-Vz0*C2)/(V0*C);
167 Aij(1,0) = /*(C3*x0-C1*z0)/(C*R0);/*/Vy0/V0;
168 Aij(1,1) = C2/C;
169 Aij(1,2) = /*y0/R0;/*/(Vz0*C1-Vx0*C3)/(V0*C);
170 Aij(2,0) = /*(C1*y0-C2*x0)/(C*R0);/*/Vz0/V0;
171 Aij(2,1) = C3/C;
172 Aij(2,2) = /*x0/R0;/*/(Vx0*C2-Vy0*C1)/(V0*C);
173 Aij.Invert();
174
175 TMatrixD Full_(3,3);
176
177 Full_ = Aij*(Pij*Zij);
178
179 //Double_t u13 = Full_(0,2);
180 //Double_t u23 = Full_(1,2);
181 //Double_t u22 = Full_(1,1);
182 //Double_t u33 = Full_(2,2);
183 //Double_t u21 = Full_(1,0);
184
185 Double_t u13 = Full_(0,0);
186 Double_t u23 = -Full_(1,0);
187 Double_t u22 = Full_(1,1);
188 Double_t u33 = Full_(2,0);
189 Double_t u21 = Full_(1,2);
190
191 Tangazh = a*atan(-u13/u33);
192 Kren = a*atan(-u23/sqrt(1 - pow(u23,2)));
193 Ryskanie = a*atan(u21/u22);
194
195 return ;
196 }
197
198
199 void InclinationInfo::Clear(){
200 //Int_t gyh = 0;
201 }
202
203
204 //ClassImp(McmdItem)
205 ClassImp(InclinationInfoI)
206 ClassImp(Quaternions)
207 ClassImp(InclinationInfo)

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