JSBSim Flight Dynamics Model 1.3.3 (16 Oct 2026)
An Open Source Flight Dynamics and Control Software Library in C++
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FGMars.cpp
1/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
2
3 Module: FGMars.cpp
4 Author: Jon Berndt
5 Date started: 1/4/04
6 Purpose: Models the Martian atmosphere very simply
7 Called by: FGFDMExec
8
9 ------------- Copyright (C) 2004 Jon S. Berndt (jon@jsbsim.org) -------------
10
11 This program is free software; you can redistribute it and/or modify it under
12 the terms of the GNU Lesser General Public License as published by the Free Software
13 Foundation; either version 2 of the License, or (at your option) any later
14 version.
15
16 This program is distributed in the hope that it will be useful, but WITHOUT
17 ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
18 FOR A PARTICULAR PURPOSE. See the GNU Lesser General Public License for more
19 details.
20
21 You should have received a copy of the GNU Lesser General Public License along with
22 this program; if not, write to the Free Software Foundation, Inc., 59 Temple
23 Place - Suite 330, Boston, MA 02111-1307, USA.
24
25 Further information about the GNU Lesser General Public License can also be found on
26 the world wide web at http://www.gnu.org.
27
28FUNCTIONAL DESCRIPTION
29--------------------------------------------------------------------------------
30Models the Martian atmosphere.
31
32HISTORY
33--------------------------------------------------------------------------------
341/04/2004 JSB Created
35
36%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
37COMMENTS, REFERENCES, and NOTES
38%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
39
40%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
41INCLUDES
42%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
43
44#include <iostream>
45
46#include "FGMars.h"
47#include "FGFDMExec.h"
48#include "input_output/FGLog.h"
49
50using namespace std;
51
52namespace JSBSim {
53
54/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
55CLASS IMPLEMENTATION
56%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
57
58
60{
61 Name = "FGMars";
62 Reng = Rstar / Mmars;
63
64 Debug(0);
65}
66
67//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
68
69void FGMars::Calculate(double altitude)
70{
71 //Calculate reftemp, refpress, and density
72
73 // LIMIT the temperatures so they do not descend below absolute zero.
74
75 if (altitude < 22960.0) {
76 Temperature = -25.68 - 0.000548*altitude + 459.67; // Convert F to Rankine
77 } else {
78 Temperature = -10.34 - 0.001217*altitude + 459.67; // Convert F to Rankine
79 }
80 Pressure = 14.62*exp(-0.00003*altitude); // psf - 14.62 psf =~ 7 millibars
81 Density = Pressure/(Reng*Temperature); // slugs/ft^3 (needs deg R. as input
82
83 //FGLogging log(LogLevel::INFO);
84 //log << "Atmosphere: h=" << altitude << " rho= " << Density << "\n";
85}
86
87//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
88// The bitmasked value choices are as follows:
89// unset: In this case (the default) JSBSim would only print
90// out the normally expected messages, essentially echoing
91// the config files as they are read. If the environment
92// variable is not set, debug_lvl is set to 1 internally
93// 0: This requests JSBSim not to output any messages
94// whatsoever.
95// 1: This value explicity requests the normal JSBSim
96// startup messages
97// 2: This value asks for a message to be printed out when
98// a class is instantiated
99// 4: When this value is set, a message is displayed when a
100// FGModel object executes its Run() method
101// 8: When this value is set, various runtime state variables
102// are printed out periodically
103// 16: When set various parameters are sanity checked and
104// a message is printed out when they go out of bounds
105
106void FGMars::Debug(int from)
107{
108 if (debug_lvl <= 0) return;
109
110 if (debug_lvl & 1) { // Standard console startup message output
111 if (from == 0) { // Constructor
112 }
113 }
114 if (debug_lvl & 2 ) { // Instantiation/Destruction notification
115 FGLogging log(LogLevel::DEBUG);
116 if (from == 0) log << "Instantiated: FGMars\n";
117 if (from == 1) log << "Destroyed: FGMars\n";
118 }
119 if (debug_lvl & 4 ) { // Run() method entry print for FGModel-derived objects
120 }
121 if (debug_lvl & 8 ) { // Runtime state variables
122 }
123 if (debug_lvl & 16) { // Sanity checking
124 }
125 if (debug_lvl & 32) { // Turbulence
126 }
127 if (debug_lvl & 64) {
128 if (from == 0) { // Constructor
129 }
130 }
131}
132
133} // namespace JSBSim
Models an empty, abstract base atmosphere class.
static constexpr double Rstar
Universal gas constant - ft*lbf/R/mol.
Encapsulates the JSBSim simulation executive.
Definition FGFDMExec.h:185
static constexpr double Mmars
Mean molecular weight of the Martian atmosphere - slug/mol.
Definition FGMars.h:76
FGMars(FGFDMExec *)
Constructor.
Definition FGMars.cpp:59
Main namespace for the JSBSim Flight Dynamics Model.
Definition FGFDMExec.cpp:73