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FGOutputTextFile.cpp
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1/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
2
3 Module: FGOutputTextFile.cpp
4 Author: Bertrand Coconnier
5 Date started: 09/17/11
6 Purpose: Manage output of sim parameters to a text file
7 Called by: FGOutput
8
9 ------------- Copyright (C) 2011 Bertrand Coconnier -------------
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
13 Software Foundation; either version 2 of the License, or (at your option) any
14 later 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
22 with this program; if not, write to the Free Software Foundation, Inc., 59
23 Temple Place - Suite 330, Boston, MA 02111-1307, USA.
24
25 Further information about the GNU Lesser General Public License can also be
26 found on the world wide web at http://www.gnu.org.
27
28FUNCTIONAL DESCRIPTION
29--------------------------------------------------------------------------------
30This is the place where you create output routines to dump data for perusal
31later.
32
33HISTORY
34--------------------------------------------------------------------------------
3509/17/11 BC Created
36
37%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
38INCLUDES
39%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
40
41#include <iomanip>
42
43#include "FGOutputTextFile.h"
44#include "models/FGAerodynamics.h"
45#include "models/FGAccelerations.h"
46#include "models/FGAtmosphere.h"
47#include "models/FGAuxiliary.h"
48#include "models/FGPropulsion.h"
49#include "models/FGMassBalance.h"
50#include "models/FGExternalReactions.h"
51#include "models/FGBuoyantForces.h"
52#include "models/FGFCS.h"
53#include "models/atmosphere/FGWinds.h"
54#include "input_output/FGXMLElement.h"
55
56using namespace std;
57
58namespace JSBSim {
59
60/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
61CLASS IMPLEMENTATION
62%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
63
64bool FGOutputTextFile::Load(Element* el)
65{
66 if(!FGOutputFile::Load(el))
67 return false;
68
69 string type = el->GetAttributeValue("type");
70 string delim;
71 if (type == "TABULAR") {
72 delim = "\t";
73 } else {
74 delim = ",";
75 }
76
77 SetDelimiter(delim);
78
79 return true;
80}
81
82//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
83
84bool FGOutputTextFile::OpenFile(void)
85{
86 datafile.clear();
87 datafile.open(Filename);
88 if (!datafile) {
89 cerr << endl << fgred << highint << "ERROR: unable to open the file "
90 << reset << Filename.c_str() << endl
91 << fgred << highint << " => Output to this file is disabled."
92 << reset << endl << endl;
93 Disable();
94 return false;
95 }
96
97 string scratch = "";
98 streambuf* buffer = datafile.rdbuf();
99 ostream outstream(buffer);
100
101 outstream.precision(10);
102
103 outstream << "Time";
104 if (SubSystems & ssSimulation) {
105 // Nothing here, yet
106 }
107 if (SubSystems & ssAerosurfaces) {
108 outstream << delimeter;
109 outstream << "Aileron Command (norm)" + delimeter;
110 outstream << "Elevator Command (norm)" + delimeter;
111 outstream << "Rudder Command (norm)" + delimeter;
112 outstream << "Flap Command (norm)" + delimeter;
113 outstream << "Left Aileron Position (deg)" + delimeter;
114 outstream << "Right Aileron Position (deg)" + delimeter;
115 outstream << "Elevator Position (deg)" + delimeter;
116 outstream << "Rudder Position (deg)" + delimeter;
117 outstream << "Flap Position (deg)";
118 }
119 if (SubSystems & ssRates) {
120 outstream << delimeter;
121 outstream << "P (deg/s)" + delimeter + "Q (deg/s)" + delimeter + "R (deg/s)" + delimeter;
122 outstream << "P dot (deg/s^2)" + delimeter + "Q dot (deg/s^2)" + delimeter + "R dot (deg/s^2)" + delimeter;
123 outstream << "P_{inertial} (deg/s)" + delimeter + "Q_{inertial} (deg/s)" + delimeter + "R_{inertial} (deg/s)";
124 }
125 if (SubSystems & ssVelocities) {
126 outstream << delimeter;
127 outstream << "q bar (psf)" + delimeter;
128 outstream << "Reynolds Number" + delimeter;
129 outstream << "V_{Total} (ft/s)" + delimeter;
130 outstream << "V_{Inertial} (ft/s)" + delimeter;
131 outstream << "UBody" + delimeter + "VBody" + delimeter + "WBody" + delimeter;
132 outstream << "UdotBody" + delimeter + "VdotBody" + delimeter + "WdotBody" + delimeter;
133 outstream << "UdotBody_i" + delimeter + "VdotBody_i" + delimeter + "WdotBody_i" + delimeter;
134 outstream << "BodyAccel_X" + delimeter + "BodyAccel_Y" + delimeter + "BodyAccel_Z" + delimeter;
135 outstream << "Aero V_{X Body} (ft/s)" + delimeter + "Aero V_{Y Body} (ft/s)" + delimeter + "Aero V_{Z Body} (ft/s)" + delimeter;
136 outstream << "V_{X_{inertial}} (ft/s)" + delimeter + "V_{Y_{inertial}} (ft/s)" + delimeter + "V_{Z_{inertial}} (ft/s)" + delimeter;
137 outstream << "V_{X_{ecef}} (ft/s)" + delimeter + "V_{Y_{ecef}} (ft/s)" + delimeter + "V_{Z_{ecef}} (ft/s)" + delimeter;
138 outstream << "V_{North} (ft/s)" + delimeter + "V_{East} (ft/s)" + delimeter + "V_{Down} (ft/s)";
139 }
140 if (SubSystems & ssForces) {
141 outstream << delimeter;
142 outstream << "F_{Drag} (lbs)" + delimeter + "F_{Side} (lbs)" + delimeter + "F_{Lift} (lbs)" + delimeter;
143 outstream << "L/D" + delimeter;
144 outstream << "F_{Aero x} (lbs)" + delimeter + "F_{Aero y} (lbs)" + delimeter + "F_{Aero z} (lbs)" + delimeter;
145 outstream << "F_{Prop x} (lbs)" + delimeter + "F_{Prop y} (lbs)" + delimeter + "F_{Prop z} (lbs)" + delimeter;
146 outstream << "F_{Gear x} (lbs)" + delimeter + "F_{Gear y} (lbs)" + delimeter + "F_{Gear z} (lbs)" + delimeter;
147 outstream << "F_{Ext x} (lbs)" + delimeter + "F_{Ext y} (lbs)" + delimeter + "F_{Ext z} (lbs)" + delimeter;
148 outstream << "F_{Buoyant x} (lbs)" + delimeter + "F_{Buoyant y} (lbs)" + delimeter + "F_{Buoyant z} (lbs)" + delimeter;
149 outstream << "F_{Weight x} (lbs)" + delimeter + "F_{Weight y} (lbs)" + delimeter + "F_{Weight z} (lbs)" + delimeter;
150 outstream << "F_{Total x} (lbs)" + delimeter + "F_{Total y} (lbs)" + delimeter + "F_{Total z} (lbs)";
151 }
152 if (SubSystems & ssMoments) {
153 outstream << delimeter;
154 outstream << "L_{Aero} (ft-lbs)" + delimeter + "M_{Aero} (ft-lbs)" + delimeter + "N_{Aero} (ft-lbs)" + delimeter;
155 outstream << "L_{Aero MRC} (ft-lbs)" + delimeter + "M_{Aero MRC} (ft-lbs)" + delimeter + "N_{Aero MRC} (ft-lbs)" + delimeter;
156 outstream << "L_{Prop} (ft-lbs)" + delimeter + "M_{Prop} (ft-lbs)" + delimeter + "N_{Prop} (ft-lbs)" + delimeter;
157 outstream << "L_{Gear} (ft-lbs)" + delimeter + "M_{Gear} (ft-lbs)" + delimeter + "N_{Gear} (ft-lbs)" + delimeter;
158 outstream << "L_{ext} (ft-lbs)" + delimeter + "M_{ext} (ft-lbs)" + delimeter + "N_{ext} (ft-lbs)" + delimeter;
159 outstream << "L_{Buoyant} (ft-lbs)" + delimeter + "M_{Buoyant} (ft-lbs)" + delimeter + "N_{Buoyant} (ft-lbs)" + delimeter;
160 outstream << "L_{Total} (ft-lbs)" + delimeter + "M_{Total} (ft-lbs)" + delimeter + "N_{Total} (ft-lbs)";
161 }
162 if (SubSystems & ssAtmosphere) {
163 outstream << delimeter;
164 outstream << "Rho (slugs/ft^3)" + delimeter;
165 outstream << "Absolute Viscosity" + delimeter;
166 outstream << "Kinematic Viscosity" + delimeter;
167 outstream << "Temperature (R)" + delimeter;
168 outstream << "P_{SL} (psf)" + delimeter;
169 outstream << "P_{Ambient} (psf)" + delimeter;
170 outstream << "Turbulence Magnitude (ft/sec)" + delimeter;
171 outstream << "Turbulence X Direction (deg)" + delimeter;
172 outstream << "Wind V_{North} (ft/s)" + delimeter + "Wind V_{East} (ft/s)" + delimeter + "Wind V_{Down} (ft/s)" + delimeter;
173 outstream << "Roll Turbulence (deg/sec)" + delimeter + "Pitch Turbulence (deg/sec)" + delimeter + "Yaw Turbulence (deg/sec)";
174 }
175 if (SubSystems & ssMassProps) {
176 outstream << delimeter;
177 outstream << "I_{xx}" + delimeter;
178 outstream << "I_{xy}" + delimeter;
179 outstream << "I_{xz}" + delimeter;
180 outstream << "I_{yx}" + delimeter;
181 outstream << "I_{yy}" + delimeter;
182 outstream << "I_{yz}" + delimeter;
183 outstream << "I_{zx}" + delimeter;
184 outstream << "I_{zy}" + delimeter;
185 outstream << "I_{zz}" + delimeter;
186 outstream << "Mass" + delimeter;
187 outstream << "Weight" + delimeter;
188 outstream << "X_{cg}" + delimeter + "Y_{cg}" + delimeter + "Z_{cg}";
189 }
190 if (SubSystems & ssPropagate) {
191 outstream << delimeter;
192 outstream << "Altitude ASL (ft)" + delimeter;
193 outstream << "Altitude AGL (ft)" + delimeter;
194 outstream << "Phi (deg)" + delimeter + "Theta (deg)" + delimeter + "Psi (deg)" + delimeter;
195 outstream << "Q(1)_{LOCAL}" + delimeter + "Q(2)_{LOCAL}" + delimeter + "Q(3)_{LOCAL}" + delimeter + "Q(4)_{LOCAL}" + delimeter;
196 outstream << "Q(1)_{ECEF}" + delimeter + "Q(2)_{ECEF}" + delimeter + "Q(3)_{ECEF}" + delimeter + "Q(4)_{ECEF}" + delimeter;
197 outstream << "Q(1)_{ECI}" + delimeter + "Q(2)_{ECI}" + delimeter + "Q(3)_{ECI}" + delimeter + "Q(4)_{ECI}" + delimeter;
198 outstream << "Alpha (deg)" + delimeter;
199 outstream << "Beta (deg)" + delimeter;
200 outstream << "Latitude (deg)" + delimeter;
201 outstream << "Latitude Geodetic (deg)" + delimeter;
202 outstream << "Longitude (deg)" + delimeter;
203 outstream << "X_{ECI} (ft)" + delimeter + "Y_{ECI} (ft)" + delimeter + "Z_{ECI} (ft)" + delimeter;
204 outstream << "X_{ECEF} (ft)" + delimeter + "Y_{ECEF} (ft)" + delimeter + "Z_{ECEF} (ft)" + delimeter;
205 outstream << "Earth Position Angle (deg)" + delimeter;
206 outstream << "Distance AGL (ft)" + delimeter;
207 outstream << "Terrain Elevation (ft)";
208 }
209 if (SubSystems & ssAeroFunctions) {
210 scratch = Aerodynamics->GetAeroFunctionStrings(delimeter);
211 if (scratch.length() != 0) outstream << delimeter << scratch;
212 }
213 if (SubSystems & ssFCS) {
214 scratch = FCS->GetComponentStrings(delimeter);
215 if (scratch.length() != 0) outstream << delimeter << scratch;
216 }
217 if (SubSystems & ssGroundReactions) {
218 outstream << delimeter;
219 outstream << GroundReactions->GetGroundReactionStrings(delimeter);
220 }
221 if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
222 outstream << delimeter;
223 outstream << Propulsion->GetPropulsionStrings(delimeter);
224 }
225
226 for (unsigned int i=0;i<OutputParameters.size();++i) {
227 if (!OutputCaptions[i].empty())
228 outstream << delimeter << OutputCaptions[i];
229 else
230 outstream << delimeter << OutputParameters[i]->GetFullyQualifiedName();
231 }
232
233 if (PreFunctions.size() > 0) {
234 for (unsigned int i=0;i<PreFunctions.size();i++) {
235 outstream << delimeter << PreFunctions[i]->GetName();
236 }
237 }
238
239 outstream << endl;
240 outstream.flush();
241
242 return true;
243}
244
245//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
246
247void FGOutputTextFile::Print(void)
248{
249 streambuf* buffer;
250 string scratch = Filename.utf8Str();
251
252 if (to_upper(scratch) == "COUT") {
253 buffer = cout.rdbuf();
254 } else {
255 buffer = datafile.rdbuf();
256 }
257
258 ostream outstream(buffer);
259
260 outstream.precision(10);
261
262 outstream << FDMExec->GetSimTime();
263 if (SubSystems & ssSimulation) {
264 }
265 if (SubSystems & ssAerosurfaces) {
266 outstream << delimeter;
267 outstream << FCS->GetDaCmd() << delimeter;
268 outstream << FCS->GetDeCmd() << delimeter;
269 outstream << FCS->GetDrCmd() << delimeter;
270 outstream << FCS->GetDfCmd() << delimeter;
271 outstream << FCS->GetDaLPos(ofDeg) << delimeter;
272 outstream << FCS->GetDaRPos(ofDeg) << delimeter;
273 outstream << FCS->GetDePos(ofDeg) << delimeter;
274 outstream << FCS->GetDrPos(ofDeg) << delimeter;
275 outstream << FCS->GetDfPos(ofDeg);
276 }
277 if (SubSystems & ssRates) {
278 outstream << delimeter;
279 outstream << (radtodeg*Propagate->GetPQR()).Dump(delimeter) << delimeter;
280 outstream << (radtodeg*Accelerations->GetPQRdot()).Dump(delimeter) << delimeter;
281 outstream << (radtodeg*Propagate->GetPQRi()).Dump(delimeter);
282 }
283 if (SubSystems & ssVelocities) {
284 outstream << delimeter;
285 outstream << Auxiliary->Getqbar() << delimeter;
286 outstream << Auxiliary->GetReynoldsNumber() << delimeter;
287 outstream << setprecision(12) << Auxiliary->GetVt() << delimeter;
288 outstream << Propagate->GetInertialVelocityMagnitude() << delimeter;
289 outstream << setprecision(12) << Propagate->GetUVW().Dump(delimeter) << delimeter;
290 outstream << setprecision(12) << Accelerations->GetUVWdot().Dump(delimeter) << delimeter;
291 outstream << setprecision(12) << Accelerations->GetUVWidot().Dump(delimeter) << delimeter;
292 outstream << setprecision(12) << Accelerations->GetBodyAccel().Dump(delimeter) << delimeter;
293 outstream << Auxiliary->GetAeroUVW().Dump(delimeter) << delimeter;
294 outstream << Propagate->GetInertialVelocity().Dump(delimeter) << delimeter;
295 outstream << Propagate->GetECEFVelocity().Dump(delimeter) << delimeter;
296 outstream << Propagate->GetVel().Dump(delimeter);
297 outstream.precision(10);
298 }
299 if (SubSystems & ssForces) {
300 outstream << delimeter;
301 outstream << Aerodynamics->GetvFw().Dump(delimeter) << delimeter;
302 outstream << Aerodynamics->GetLoD() << delimeter;
303 outstream << Aerodynamics->GetForces().Dump(delimeter) << delimeter;
304 outstream << Propulsion->GetForces().Dump(delimeter) << delimeter;
305 outstream << Accelerations->GetGroundForces().Dump(delimeter) << delimeter;
306 outstream << ExternalReactions->GetForces().Dump(delimeter) << delimeter;
307 outstream << BuoyantForces->GetForces().Dump(delimeter) << delimeter;
308 outstream << Accelerations->GetWeight().Dump(delimeter) << delimeter;
309 outstream << Accelerations->GetForces().Dump(delimeter);
310 }
311 if (SubSystems & ssMoments) {
312 outstream << delimeter;
313 outstream << Aerodynamics->GetMoments().Dump(delimeter) << delimeter;
314 outstream << Aerodynamics->GetMomentsMRC().Dump(delimeter) << delimeter;
315 outstream << Propulsion->GetMoments().Dump(delimeter) << delimeter;
316 outstream << Accelerations->GetGroundMoments().Dump(delimeter) << delimeter;
317 outstream << ExternalReactions->GetMoments().Dump(delimeter) << delimeter;
318 outstream << BuoyantForces->GetMoments().Dump(delimeter) << delimeter;
319 outstream << Accelerations->GetMoments().Dump(delimeter);
320 }
321 if (SubSystems & ssAtmosphere) {
322 outstream << delimeter;
323 outstream << Atmosphere->GetDensity() << delimeter;
324 outstream << Atmosphere->GetAbsoluteViscosity() << delimeter;
325 outstream << Atmosphere->GetKinematicViscosity() << delimeter;
326 outstream << Atmosphere->GetTemperature() << delimeter;
327 outstream << Atmosphere->GetPressureSL() << delimeter;
328 outstream << Atmosphere->GetPressure() << delimeter;
329 outstream << Winds->GetTurbMagnitude() << delimeter;
330 outstream << Winds->GetTurbDirection() << delimeter;
331 outstream << Winds->GetTotalWindNED().Dump(delimeter) << delimeter;
332 outstream << (Winds->GetTurbPQR()*radtodeg).Dump(delimeter);
333 }
334 if (SubSystems & ssMassProps) {
335 outstream << delimeter;
336 outstream << MassBalance->GetJ().Dump(delimeter) << delimeter;
337 outstream << MassBalance->GetMass() << delimeter;
338 outstream << MassBalance->GetWeight() << delimeter;
339 outstream << MassBalance->GetXYZcg().Dump(delimeter);
340 }
341 if (SubSystems & ssPropagate) {
342 outstream.precision(14);
343 outstream << delimeter;
344 outstream << Propagate->GetAltitudeASL() << delimeter;
345 outstream << Propagate->GetDistanceAGL() << delimeter;
346 outstream << (radtodeg*Propagate->GetEuler()).Dump(delimeter) << delimeter;
347 outstream << Propagate->GetQuaternion().Dump(delimeter) << delimeter;
348 FGQuaternion Qec = Propagate->GetQuaternionECEF();
349 outstream << Qec.Dump(delimeter) << delimeter;
350 outstream << Propagate->GetQuaternionECI().Dump(delimeter) << delimeter;
351 outstream << Auxiliary->Getalpha(inDegrees) << delimeter;
352 outstream << Auxiliary->Getbeta(inDegrees) << delimeter;
353 outstream << Propagate->GetLatitudeDeg() << delimeter;
354 outstream << Propagate->GetGeodLatitudeDeg() << delimeter;
355 outstream << Propagate->GetLongitudeDeg() << delimeter;
356 outstream.precision(18);
357 outstream << ((FGColumnVector3)Propagate->GetInertialPosition()).Dump(delimeter) << delimeter;
358 outstream << ((FGColumnVector3)Propagate->GetLocation()).Dump(delimeter) << delimeter;
359 outstream.precision(14);
360 outstream << Propagate->GetEarthPositionAngleDeg() << delimeter;
361 outstream << Propagate->GetDistanceAGL() << delimeter;
362 outstream << Propagate->GetTerrainElevation();
363 outstream.precision(10);
364 }
365 if (SubSystems & ssAeroFunctions) {
366 scratch = Aerodynamics->GetAeroFunctionValues(delimeter);
367 if (scratch.length() != 0) outstream << delimeter << scratch;
368 }
369 if (SubSystems & ssFCS) {
370 scratch = FCS->GetComponentValues(delimeter);
371 if (scratch.length() != 0) outstream << delimeter << scratch;
372 }
373 if (SubSystems & ssGroundReactions) {
374 outstream << delimeter;
375 outstream << GroundReactions->GetGroundReactionValues(delimeter);
376 }
377 if (SubSystems & ssPropulsion && Propulsion->GetNumEngines() > 0) {
378 outstream << delimeter;
379 outstream << Propulsion->GetPropulsionValues(delimeter);
380 }
381
382 outstream.precision(18);
383 for (unsigned int i=0;i<OutputParameters.size();++i) {
384 outstream << delimeter << OutputParameters[i]->GetValue();
385 }
386 for (unsigned int i=0;i<PreFunctions.size();i++) {
387 outstream << delimeter << PreFunctions[i]->getDoubleValue();
388 }
389 outstream.precision(10);
390
391 outstream << endl;
392 outstream.flush();
393}
394}
i
#define i(x)
JSBSim::Element::GetAttributeValue
std::string GetAttributeValue(const std::string &key)
Retrieves an attribute.
Definition FGXMLElement.cpp:260
JSBSim::FGColumnVector3
This class implements a 3 element column vector.
Definition FGColumnVector3.h:64
JSBSim::FGJSBBase::radtodeg
static constexpr double radtodeg
Definition FGJSBBase.h:348
JSBSim::FGJSBBase::highint
static char highint[5]
highlights text
Definition FGJSBBase.h:123
JSBSim::FGJSBBase::reset
static char reset[5]
resets text properties
Definition FGJSBBase.h:129
JSBSim::FGJSBBase::fgred
static char fgred[6]
red text
Definition FGJSBBase.h:139
JSBSim::FGModelFunctions::PreFunctions
std::vector< FGFunction * > PreFunctions
Definition FGModelFunctions.h:100
JSBSim::FGModel::FDMExec
FGFDMExec * FDMExec
Definition FGModel.h:116
JSBSim::FGOutputFile::Load
bool Load(Element *el) override
Init the output directives from an XML file.
Definition FGOutputFile.cpp:95
JSBSim::FGOutputTextFile::OpenFile
bool OpenFile(void) override
Opens the file.
Definition FGOutputTextFile.cpp:84
JSBSim::FGOutputTextFile::Print
void Print(void) override
Generates the output to the text file.
Definition FGOutputTextFile.cpp:247
JSBSim::FGOutputTextFile::Load
bool Load(Element *el) override
Init the output directives from an XML file.
Definition FGOutputTextFile.cpp:64
JSBSim::FGOutputTextFile::SetDelimiter
void SetDelimiter(const std::string &delim)
Set the delimiter.
Definition FGOutputTextFile.h:75
JSBSim::FGOutputType::ssGroundReactions
@ ssGroundReactions
Subsystem: Ground Reactions (= 1024)
Definition FGOutputType.h:186
JSBSim::FGOutputType::ssMoments
@ ssMoments
Subsystem: Moments (= 32)
Definition FGOutputType.h:181
JSBSim::FGOutputType::ssPropagate
@ ssPropagate
Subsystem: Propagate (= 512)
Definition FGOutputType.h:185
JSBSim::FGOutputType::ssPropulsion
@ ssPropulsion
Subsystem: Propulsion (= 4096)
Definition FGOutputType.h:188
JSBSim::FGOutputType::ssSimulation
@ ssSimulation
Subsystem: Simulation (= 1)
Definition FGOutputType.h:176
JSBSim::FGOutputType::ssForces
@ ssForces
Subsystem: Forces (= 16)
Definition FGOutputType.h:180
JSBSim::FGOutputType::ssAerosurfaces
@ ssAerosurfaces
Subsystem: Aerosurfaces (= 2)
Definition FGOutputType.h:177
JSBSim::FGOutputType::ssMassProps
@ ssMassProps
Subsystem: Mass Properties (= 128)
Definition FGOutputType.h:183
JSBSim::FGOutputType::ssFCS
@ ssFCS
Subsystem: FCS (= 2048)
Definition FGOutputType.h:187
JSBSim::FGOutputType::ssRates
@ ssRates
Subsystem: Body rates (= 4)
Definition FGOutputType.h:178
JSBSim::FGOutputType::ssAtmosphere
@ ssAtmosphere
Subsystem: Atmosphere (= 64)
Definition FGOutputType.h:182
JSBSim::FGOutputType::ssAeroFunctions
@ ssAeroFunctions
Subsystem: Coefficients (= 256)
Definition FGOutputType.h:184
JSBSim::FGOutputType::ssVelocities
@ ssVelocities
Subsystem: Velocities (= 8)
Definition FGOutputType.h:179
JSBSim::FGOutputType::GroundReactions
FGGroundReactions * GroundReactions
Definition FGOutputType.h:208
JSBSim::FGOutputType::OutputParameters
std::vector< FGPropertyValue * > OutputParameters
Definition FGOutputType.h:194
JSBSim::FGOutputType::Disable
void Disable(void)
Disables the output generation.
Definition FGOutputType.h:168
JSBSim::FGOutputType::Accelerations
FGAccelerations * Accelerations
Definition FGOutputType.h:206
JSBSim::FGOutputType::Propulsion
FGPropulsion * Propulsion
Definition FGOutputType.h:203
JSBSim::FGOutputType::Auxiliary
FGAuxiliary * Auxiliary
Definition FGOutputType.h:199
JSBSim::FGOutputType::Propagate
FGPropagate * Propagate
Definition FGOutputType.h:205
JSBSim::FGOutputType::ExternalReactions
FGExternalReactions * ExternalReactions
Definition FGOutputType.h:209
JSBSim::FGOutputType::Atmosphere
FGAtmosphere * Atmosphere
Definition FGOutputType.h:201
JSBSim::FGOutputType::MassBalance
FGMassBalance * MassBalance
Definition FGOutputType.h:204
JSBSim::FGOutputType::OutputCaptions
std::vector< std::string > OutputCaptions
Definition FGOutputType.h:195
JSBSim::FGOutputType::Aerodynamics
FGAerodynamics * Aerodynamics
Definition FGOutputType.h:198
JSBSim::FGOutputType::BuoyantForces
FGBuoyantForces * BuoyantForces
Definition FGOutputType.h:210
JSBSim::FGQuaternion
Models the Quaternion representation of rotations.
Definition FGQuaternion.h:86
JSBSim::FGQuaternion::Dump
std::string Dump(const std::string &delimiter) const
Definition FGQuaternion.cpp:239
JSBSim::ofDeg
@ ofDeg
Definition FGFCS.h:56
to_upper
std::string & to_upper(std::string &str)