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Update to the latest version of JSBSim which supports Lighter Than Air craft
[flightgear.git] / src / FDM / JSBSim / FGState.cpp
1 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
2
3  Module:       FGState.cpp
4  Author:       Jon Berndt
5  Date started: 11/17/98
6  Called by:    FGFDMExec and accessed by all models.
7
8  ------------- Copyright (C) 1999  Jon S. Berndt (jsb@hal-pc.org) -------------
9
10  This program is free software; you can redistribute it and/or modify it under
11  the terms of the GNU Lesser General Public License as published by the Free Software
12  Foundation; either version 2 of the License, or (at your option) any later
13  version.
14
15  This program is distributed in the hope that it will be useful, but WITHOUT
16  ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
17  FOR A PARTICULAR PURPOSE.  See the GNU Lesser General Public License for more
18  details.
19
20  You should have received a copy of the GNU Lesser General Public License along with
21  this program; if not, write to the Free Software Foundation, Inc., 59 Temple
22  Place - Suite 330, Boston, MA  02111-1307, USA.
23
24  Further information about the GNU Lesser General Public License can also be found on
25  the world wide web at http://www.gnu.org.
26
27 FUNCTIONAL DESCRIPTION
28 --------------------------------------------------------------------------------
29 See header file.
30
31 HISTORY
32 --------------------------------------------------------------------------------
33 11/17/98   JSB   Created
34
35 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
36 INCLUDES
37 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
38
39 #ifdef FGFS
40 #  include <simgear/compiler.h>
41 #  include <math.h>
42 #else
43 #  if defined(sgi) && !defined(__GNUC__)
44 #    include <math.h>
45 #  else
46 #    include <cmath>
47 #  endif
48 #endif
49
50 #include "FGState.h"
51
52 namespace JSBSim {
53
54 static const char *IdSrc = "$Id$";
55 static const char *IdHdr = ID_STATE;
56
57 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
58 MACROS
59 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
60
61 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
62 CLASS IMPLEMENTATION
63 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
64
65 FGState::FGState(FGFDMExec* fdex)
66 {
67   FDMExec = fdex;
68
69   sim_time = 0.0;
70   dt = 1.0/120.0;
71
72   Aircraft     = FDMExec->GetAircraft();
73   Propagate    = FDMExec->GetPropagate();
74   Auxiliary    = FDMExec->GetAuxiliary();
75   FCS          = FDMExec->GetFCS();
76   Atmosphere   = FDMExec->GetAtmosphere();
77   Aerodynamics = FDMExec->GetAerodynamics();
78   GroundReactions = FDMExec->GetGroundReactions();
79   Propulsion      = FDMExec->GetPropulsion();
80   PropertyManager = FDMExec->GetPropertyManager();
81
82   bind();
83
84   Debug(0);
85 }
86
87 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
88
89 FGState::~FGState()
90 {
91   Debug(1);
92 }
93
94 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
95
96 void FGState::Initialize(FGInitialCondition *FGIC)
97 {
98   sim_time = 0.0;
99
100   Propagate->SetInitialState( FGIC );
101
102   Atmosphere->Run();
103   Atmosphere->SetWindNED( FGIC->GetWindNFpsIC(),
104                           FGIC->GetWindEFpsIC(),
105                           FGIC->GetWindDFpsIC() );
106
107   FGColumnVector3 vAeroUVW;
108   vAeroUVW = Propagate->GetUVW() + Propagate->GetTl2b()*Atmosphere->GetWindNED();
109
110   double alpha, beta;
111   if (vAeroUVW(eW) != 0.0)
112     alpha = vAeroUVW(eU)*vAeroUVW(eU) > 0.0 ? atan2(vAeroUVW(eW), vAeroUVW(eU)) : 0.0;
113   else
114     alpha = 0.0;
115   if (vAeroUVW(eV) != 0.0)
116     beta = vAeroUVW(eU)*vAeroUVW(eU)+vAeroUVW(eW)*vAeroUVW(eW) > 0.0 ? atan2(vAeroUVW(eV), (fabs(vAeroUVW(eU))/vAeroUVW(eU))*sqrt(vAeroUVW(eU)*vAeroUVW(eU) + vAeroUVW(eW)*vAeroUVW(eW))) : 0.0;
117   else
118     beta = 0.0;
119
120   Auxiliary->SetAB(alpha, beta);
121
122   double Vt = vAeroUVW.Magnitude();
123   Auxiliary->SetVt(Vt);
124
125   Auxiliary->SetMach(Vt/Atmosphere->GetSoundSpeed());
126
127   double qbar = 0.5*Vt*Vt*Atmosphere->GetDensity();
128   Auxiliary->Setqbar(qbar);
129 }
130
131 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
132
133 void FGState::bind(void)
134 {
135   PropertyManager->Tie("sim-time-sec", this, &FGState::Getsim_time);
136 }
137
138 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
139 //    The bitmasked value choices are as follows:
140 //    unset: In this case (the default) JSBSim would only print
141 //       out the normally expected messages, essentially echoing
142 //       the config files as they are read. If the environment
143 //       variable is not set, debug_lvl is set to 1 internally
144 //    0: This requests JSBSim not to output any messages
145 //       whatsoever.
146 //    1: This value explicity requests the normal JSBSim
147 //       startup messages
148 //    2: This value asks for a message to be printed out when
149 //       a class is instantiated
150 //    4: When this value is set, a message is displayed when a
151 //       FGModel object executes its Run() method
152 //    8: When this value is set, various runtime state variables
153 //       are printed out periodically
154 //    16: When set various parameters are sanity checked and
155 //       a message is printed out when they go out of bounds
156
157 void FGState::Debug(int from)
158 {
159   if (debug_lvl <= 0) return;
160
161   if (debug_lvl & 1) { // Standard console startup message output
162     if (from == 0) { // Constructor
163
164     }
165   }
166   if (debug_lvl & 2 ) { // Instantiation/Destruction notification
167     if (from == 0) cout << "Instantiated: FGState" << endl;
168     if (from == 1) cout << "Destroyed:    FGState" << endl;
169   }
170   if (debug_lvl & 4 ) { // Run() method entry print for FGModel-derived objects
171   }
172   if (debug_lvl & 8 ) { // Runtime state variables
173   }
174   if (debug_lvl & 16) { // Sanity checking
175   }
176   if (debug_lvl & 64) {
177     if (from == 0) { // Constructor
178       cout << IdSrc << endl;
179       cout << IdHdr << endl;
180     }
181   }
182 }
183 }