1 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
3 Module: FGAerodynamics.cpp
6 Purpose: Encapsulates the aerodynamic forces (gear and collision)
8 ------------- Copyright (C) 2000 Jon S. Berndt (jsb@hal-pc.org) -------------
10 This program is free software; you can redistribute it and/or modify it under
11 the terms of the GNU General Public License as published by the Free Software
12 Foundation; either version 2 of the License, or (at your option) any later
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 General Public License for more
20 You should have received a copy of the GNU 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.
24 Further information about the GNU General Public License can also be found on
25 the world wide web at http://www.gnu.org.
27 FUNCTIONAL DESCRIPTION
28 --------------------------------------------------------------------------------
31 --------------------------------------------------------------------------------
33 04/22/01 JSB Moved code into here from FGAircraft
35 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
37 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
39 #include "FGAerodynamics.h"
41 static const char *IdSrc = "$Id$";
42 static const char *IdHdr = ID_AERODYNAMICS;
44 extern short debug_lvl;
46 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
48 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
51 FGAerodynamics::FGAerodynamics(FGFDMExec* FDMExec) : FGModel(FDMExec),
58 Name = "FGAerodynamics";
67 Coeff = new CoeffArray[6];
69 if (debug_lvl & 2) cout << "Instantiated: FGAerodynamics" << endl;
72 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
74 FGAerodynamics::~FGAerodynamics()
78 for (j=0; j<Coeff[i].size(); j++) {
84 if (debug_lvl & 2) cout << "Destroyed: FGAerodynamics" << endl;
87 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
89 bool FGAerodynamics::Run(void)
92 unsigned int axis_ctr,ctr;
94 if (!FGModel::Run()) {
96 alpha = Translation->Getalpha();
97 beta = Translation->Getbeta();
102 for (axis_ctr = 0; axis_ctr < 3; axis_ctr++) {
103 for (ctr=0; ctr < Coeff[axis_ctr].size(); ctr++) {
104 vFs(axis_ctr+1) += Coeff[axis_ctr][ctr]->TotalValue();
108 vForces = State->GetTs2b(alpha, beta)*vFs;
110 // see http://home.earthlink.net/~apeden/jsbsim_moments_due_to_forces.txt
111 // for details on this
113 vDXYZcg(eX) = -(Aircraft->GetXYZrp(eX) - MassBalance->GetXYZcg(eX))/12.0;
114 vDXYZcg(eY) = (Aircraft->GetXYZrp(eY) - MassBalance->GetXYZcg(eY))/12.0;
115 vDXYZcg(eZ) = -(Aircraft->GetXYZrp(eZ) - MassBalance->GetXYZcg(eZ))/12.0;
117 vMoments(eL) = vForces(eZ)*vDXYZcg(eY) - vForces(eY)*vDXYZcg(eZ);
118 vMoments(eM) = vForces(eX)*vDXYZcg(eZ) - vForces(eZ)*vDXYZcg(eX);
119 vMoments(eN) = vForces(eY)*vDXYZcg(eX) - vForces(eX)*vDXYZcg(eY);
121 for (axis_ctr = 0; axis_ctr < 3; axis_ctr++) {
122 for (ctr = 0; ctr < Coeff[axis_ctr+3].size(); ctr++) {
123 vMoments(axis_ctr+1) += Coeff[axis_ctr+3][ctr]->TotalValue();
132 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
134 bool FGAerodynamics::Load(FGConfigFile* AC_cfg)
138 AC_cfg->GetNextConfigLine();
140 while ((token = AC_cfg->GetValue()) != "/AERODYNAMICS") {
141 if (token == "AXIS") {
143 axis = AC_cfg->GetValue("NAME");
144 AC_cfg->GetNextConfigLine();
145 while ((token = AC_cfg->GetValue()) != "/AXIS") {
146 ca.push_back(new FGCoefficient(FDMExec, AC_cfg));
147 if (debug_lvl > 0) DisplayCoeffFactors(ca.back()->Getmultipliers());
149 Coeff[AxisIdx[axis]] = ca;
150 AC_cfg->GetNextConfigLine();
157 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
159 void FGAerodynamics::DisplayCoeffFactors(vector <eParam> multipliers)
163 cout << " Non-Dimensionalized by: ";
165 for (i=0; i<multipliers.size();i++) cout << State->paramdef[multipliers[i]];
170 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
172 string FGAerodynamics::GetCoefficientStrings(void)
174 string CoeffStrings = "";
175 bool firstime = true;
176 unsigned int axis, sd;
178 for (axis = 0; axis < 6; axis++) {
179 for (sd = 0; sd < Coeff[axis].size(); sd++) {
183 CoeffStrings += ", ";
185 CoeffStrings += Coeff[axis][sd]->Getname();
191 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
193 string FGAerodynamics::GetCoefficientValues(void)
195 string SDValues = "";
197 bool firstime = true;
199 for (unsigned int axis = 0; axis < 6; axis++) {
200 for (unsigned int sd = 0; sd < Coeff[axis].size(); sd++) {
206 sprintf(buffer, "%9.6f", Coeff[axis][sd]->GetSD());
207 SDValues += string(buffer);
214 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
216 float FGAerodynamics::GetNlf(void)
218 if (fabs(Position->GetGamma()) < 1.57) {
219 return (vFs(eZ)/(MassBalance->GetWeight()*cos(Position->GetGamma())));
225 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
227 float FGAerodynamics::GetLoD(void)
231 if (vFs(1) != 0.00) return vFs(3)/vFs(1);
235 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
237 void FGAerodynamics::Debug(void)
239 //TODO: Add your source code here