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JSBSim Flight Dynamics Model 1.0 (23 February 2013)
An Open Source Flight Dynamics and Control Software Library in C++
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00001 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00002 00003 Module: FGJSBBase.cpp 00004 Author: Jon S. Berndt 00005 Date started: 07/01/01 00006 Purpose: Encapsulates the JSBBase object 00007 00008 ------------- Copyright (C) 2001 Jon S. Berndt (jon@jsbsim.org) ------------- 00009 00010 This program is free software; you can redistribute it and/or modify it under 00011 the terms of the GNU Lesser General Public License as published by the Free Software 00012 Foundation; either version 2 of the License, or (at your option) any later 00013 version. 00014 00015 This program is distributed in the hope that it will be useful, but WITHOUT 00016 ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS 00017 FOR A PARTICULAR PURPOSE. See the GNU Lesser General Public License for more 00018 details. 00019 00020 You should have received a copy of the GNU Lesser General Public License along with 00021 this program; if not, write to the Free Software Foundation, Inc., 59 Temple 00022 Place - Suite 330, Boston, MA 02111-1307, USA. 00023 00024 Further information about the GNU Lesser General Public License can also be found on 00025 the world wide web at http://www.gnu.org. 00026 00027 FUNCTIONAL DESCRIPTION 00028 -------------------------------------------------------------------------------- 00029 00030 HISTORY 00031 -------------------------------------------------------------------------------- 00032 07/01/01 JSB Created 00033 00034 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00035 INCLUDES 00036 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/ 00037 00038 #define BASE 00039 00040 #include "FGJSBBase.h" 00041 #include <iostream> 00042 #include <sstream> 00043 #include <cstdlib> 00044 00045 namespace JSBSim { 00046 00047 static const char *IdSrc = "$Id: FGJSBBase.cpp,v 1.36 2013/01/25 13:39:11 jberndt Exp $"; 00048 static const char *IdHdr = ID_JSBBASE; 00049 00050 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00051 CLASS IMPLEMENTATION 00052 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/ 00053 00054 #ifndef _MSC_VER 00055 char FGJSBBase::highint[5] = {27, '[', '1', 'm', '\0' }; 00056 char FGJSBBase::halfint[5] = {27, '[', '2', 'm', '\0' }; 00057 char FGJSBBase::normint[6] = {27, '[', '2', '2', 'm', '\0' }; 00058 char FGJSBBase::reset[5] = {27, '[', '0', 'm', '\0' }; 00059 char FGJSBBase::underon[5] = {27, '[', '4', 'm', '\0' }; 00060 char FGJSBBase::underoff[6] = {27, '[', '2', '4', 'm', '\0' }; 00061 char FGJSBBase::fgblue[6] = {27, '[', '3', '4', 'm', '\0' }; 00062 char FGJSBBase::fgcyan[6] = {27, '[', '3', '6', 'm', '\0' }; 00063 char FGJSBBase::fgred[6] = {27, '[', '3', '1', 'm', '\0' }; 00064 char FGJSBBase::fggreen[6] = {27, '[', '3', '2', 'm', '\0' }; 00065 char FGJSBBase::fgdef[6] = {27, '[', '3', '9', 'm', '\0' }; 00066 #else 00067 char FGJSBBase::highint[5] = {'\0' }; 00068 char FGJSBBase::halfint[5] = {'\0' }; 00069 char FGJSBBase::normint[6] = {'\0' }; 00070 char FGJSBBase::reset[5] = {'\0' }; 00071 char FGJSBBase::underon[5] = {'\0' }; 00072 char FGJSBBase::underoff[6] = {'\0' }; 00073 char FGJSBBase::fgblue[6] = {'\0' }; 00074 char FGJSBBase::fgcyan[6] = {'\0' }; 00075 char FGJSBBase::fgred[6] = {'\0' }; 00076 char FGJSBBase::fggreen[6] = {'\0' }; 00077 char FGJSBBase::fgdef[6] = {'\0' }; 00078 #endif 00079 00080 const double FGJSBBase::radtodeg = 57.295779513082320876798154814105; 00081 const double FGJSBBase::degtorad = 0.017453292519943295769236907684886; 00082 const double FGJSBBase::hptoftlbssec = 550.0; 00083 const double FGJSBBase::psftoinhg = 0.014138; 00084 const double FGJSBBase::psftopa = 47.88; 00085 const double FGJSBBase::fpstokts = 0.592484; 00086 const double FGJSBBase::ktstofps = 1.68781; 00087 const double FGJSBBase::inchtoft = 0.08333333; 00088 const double FGJSBBase::in3tom3 = 1.638706E-5; 00089 const double FGJSBBase::m3toft3 = 1.0/(fttom*fttom*fttom); 00090 const double FGJSBBase::inhgtopa = 3386.38; 00091 const double FGJSBBase::fttom = 0.3048; 00092 double FGJSBBase::Reng = 1716.56; // Gas constant for Air (ft-lb/slug-R) 00093 double FGJSBBase::Rstar = 1545.348; // Universal gas constant 00094 double FGJSBBase::Mair = 28.9645; // 00095 const double FGJSBBase::SHRatio = 1.40; 00096 00097 // Note that definition of lbtoslug by the inverse of slugtolb and not 00098 // to a different constant you can also get from some tables will make 00099 // lbtoslug*slugtolb == 1 up to the magnitude of roundoff. So converting from 00100 // slug to lb and back will yield to the original value you started with up 00101 // to the magnitude of roundoff. 00102 // Taken from units gnu commandline tool 00103 const double FGJSBBase::slugtolb = 32.174049; 00104 const double FGJSBBase::lbtoslug = 1.0/slugtolb; 00105 const double FGJSBBase::kgtolb = 2.20462; 00106 const double FGJSBBase::kgtoslug = 0.06852168; 00107 00108 const string FGJSBBase::needed_cfg_version = "2.0"; 00109 const string FGJSBBase::JSBSim_version = "1.0 " __DATE__ " " __TIME__ ; 00110 00111 std::queue <FGJSBBase::Message> FGJSBBase::Messages; 00112 FGJSBBase::Message FGJSBBase::localMsg; 00113 unsigned int FGJSBBase::messageId = 0; 00114 00115 short FGJSBBase::debug_lvl = 1; 00116 00117 using std::cerr; 00118 using std::cout; 00119 using std::endl; 00120 00121 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00122 00123 void FGJSBBase::PutMessage(const Message& msg) 00124 { 00125 Messages.push(msg); 00126 } 00127 00128 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00129 00130 void FGJSBBase::PutMessage(const string& text) 00131 { 00132 Message msg; 00133 msg.text = text; 00134 msg.messageId = messageId++; 00135 msg.subsystem = "FDM"; 00136 msg.type = Message::eText; 00137 Messages.push(msg); 00138 } 00139 00140 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00141 00142 void FGJSBBase::PutMessage(const string& text, bool bVal) 00143 { 00144 Message msg; 00145 msg.text = text; 00146 msg.messageId = messageId++; 00147 msg.subsystem = "FDM"; 00148 msg.type = Message::eBool; 00149 msg.bVal = bVal; 00150 Messages.push(msg); 00151 } 00152 00153 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00154 00155 void FGJSBBase::PutMessage(const string& text, int iVal) 00156 { 00157 Message msg; 00158 msg.text = text; 00159 msg.messageId = messageId++; 00160 msg.subsystem = "FDM"; 00161 msg.type = Message::eInteger; 00162 msg.iVal = iVal; 00163 Messages.push(msg); 00164 } 00165 00166 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00167 00168 void FGJSBBase::PutMessage(const string& text, double dVal) 00169 { 00170 Message msg; 00171 msg.text = text; 00172 msg.messageId = messageId++; 00173 msg.subsystem = "FDM"; 00174 msg.type = Message::eDouble; 00175 msg.dVal = dVal; 00176 Messages.push(msg); 00177 } 00178 00179 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00180 00181 int FGJSBBase::SomeMessages(void) 00182 { 00183 return !Messages.empty(); 00184 } 00185 00186 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00187 00188 void FGJSBBase::ProcessMessage(void) 00189 { 00190 if (Messages.empty()) return; 00191 localMsg = Messages.front(); 00192 00193 while (Messages.size() > 0) { 00194 switch (localMsg.type) { 00195 case JSBSim::FGJSBBase::Message::eText: 00196 cout << localMsg.messageId << ": " << localMsg.text << endl; 00197 break; 00198 case JSBSim::FGJSBBase::Message::eBool: 00199 cout << localMsg.messageId << ": " << localMsg.text << " " << localMsg.bVal << endl; 00200 break; 00201 case JSBSim::FGJSBBase::Message::eInteger: 00202 cout << localMsg.messageId << ": " << localMsg.text << " " << localMsg.iVal << endl; 00203 break; 00204 case JSBSim::FGJSBBase::Message::eDouble: 00205 cout << localMsg.messageId << ": " << localMsg.text << " " << localMsg.dVal << endl; 00206 break; 00207 default: 00208 cerr << "Unrecognized message type." << endl; 00209 break; 00210 } 00211 Messages.pop(); 00212 if (Messages.size() > 0) localMsg = Messages.front(); 00213 else break; 00214 } 00215 00216 } 00217 00218 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00219 00220 FGJSBBase::Message* FGJSBBase::ProcessNextMessage(void) 00221 { 00222 if (Messages.empty()) return NULL; 00223 localMsg = Messages.front(); 00224 00225 Messages.pop(); 00226 return &localMsg; 00227 } 00228 00229 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00230 00231 void FGJSBBase::disableHighLighting(void) 00232 { 00233 highint[0]='\0'; 00234 halfint[0]='\0'; 00235 normint[0]='\0'; 00236 reset[0]='\0'; 00237 underon[0]='\0'; 00238 underoff[0]='\0'; 00239 fgblue[0]='\0'; 00240 fgcyan[0]='\0'; 00241 fgred[0]='\0'; 00242 fggreen[0]='\0'; 00243 fgdef[0]='\0'; 00244 } 00245 00246 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00247 00248 string FGJSBBase::CreateIndexedPropertyName(const string& Property, int index) 00249 { 00250 std::ostringstream buf; 00251 buf << Property << '[' << index << ']'; 00252 return buf.str(); 00253 } 00254 00255 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00256 00257 double FGJSBBase::GaussianRandomNumber(void) 00258 { 00259 static double V1, V2, S; 00260 static int phase = 0; 00261 double X; 00262 00263 if (phase == 0) { 00264 V1 = V2 = S = X = 0.0; 00265 00266 do { 00267 double U1 = (double)rand() / RAND_MAX; 00268 double U2 = (double)rand() / RAND_MAX; 00269 00270 V1 = 2 * U1 - 1; 00271 V2 = 2 * U2 - 1; 00272 S = V1 * V1 + V2 * V2; 00273 } while(S >= 1 || S == 0); 00274 00275 X = V1 * sqrt(-2 * log(S) / S); 00276 } else 00277 X = V2 * sqrt(-2 * log(S) / S); 00278 00279 phase = 1 - phase; 00280 00281 return X; 00282 } 00283 00284 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00285 00286 double FGJSBBase::VcalibratedFromMach(double mach, double p, double psl, double rhosl) 00287 { 00288 double pt,A; 00289 00290 if (mach < 0) mach=0; 00291 if (mach < 1) //calculate total pressure assuming isentropic flow 00292 pt=p*pow((1 + 0.2*mach*mach),3.5); 00293 else { 00294 // shock in front of pitot tube, we'll assume its normal and use 00295 // the Rayleigh Pitot Tube Formula, i.e. the ratio of total 00296 // pressure behind the shock to the static pressure in front of 00297 // the normal shock assumption should not be a bad one -- most supersonic 00298 // aircraft place the pitot probe out front so that it is the forward 00299 // most point on the aircraft. The real shock would, of course, take 00300 // on something like the shape of a rounded-off cone but, here again, 00301 // the assumption should be good since the opening of the pitot probe 00302 // is very small and, therefore, the effects of the shock curvature 00303 // should be small as well. AFAIK, this approach is fairly well accepted 00304 // within the aerospace community 00305 00306 // The denominator below is zero for Mach ~ 0.38, for which 00307 // we'll never be here, so we're safe 00308 00309 pt = p*166.92158*pow(mach,7.0)/pow(7*mach*mach-1,2.5); 00310 } 00311 00312 A = pow(((pt-p)/psl+1),0.28571); 00313 return sqrt(7*psl/rhosl*(A-1)); 00314 } 00315 00316 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00317 00318 double FGJSBBase::MachFromVcalibrated(double vcas, double p, double psl, double rhosl) 00319 { 00320 double pt = p + psl*(pow(1+vcas*vcas*rhosl/(7.0*psl),3.5)-1); 00321 00322 if (pt/p < 1.89293) 00323 return sqrt(5.0*(pow(pt/p, 0.2857143) -1)); // Mach < 1 00324 else { 00325 // Mach >= 1 00326 double mach = sqrt(0.77666*pt/p); // Initial guess is based on a quadratic approximation of the Rayleigh formula 00327 double delta = 1.; 00328 double target = pt/(166.92158*p); 00329 int iter = 0; 00330 00331 // Find the root with Newton-Raphson. Since the differential is never zero, 00332 // the function is monotonic and has only one root with a multiplicity of one. 00333 // Convergence is certain. 00334 while (delta > 1E-5 && iter < 10) { 00335 double m2 = mach*mach; // Mach^2 00336 double m6 = m2*m2*m2; // Mach^6 00337 delta = mach*m6/pow(7.0*m2-1.0,2.5) - target; 00338 double diff = 7.0*m6*(2.0*m2-1)/pow(7.0*m2-1.0,3.5); // Never zero when Mach >= 1 00339 mach -= delta/diff; 00340 iter++; 00341 } 00342 00343 return mach; 00344 } 00345 } 00346 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% 00347 00348 } // namespace JSBSim 00349