108     outstream << delimeter;  in OpenFile()
109     outstream << "Aileron Command (norm)" + delimeter;  in OpenFile()
110     outstream << "Elevator Command (norm)" + delimeter;  in OpenFile()
111     outstream << "Rudder Command (norm)" + delimeter;  in OpenFile()
112     outstream << "Flap Command (norm)" + delimeter;  in OpenFile()
113     outstream << "Left Aileron Position (deg)" + delimeter;  in OpenFile()
114     outstream << "Right Aileron Position (deg)" + delimeter;  in OpenFile()
115     outstream << "Elevator Position (deg)" + delimeter;  in OpenFile()
116     outstream << "Rudder Position (deg)" + delimeter;  in OpenFile()
120     outstream << delimeter;  in OpenFile()
121     outstream << "P (deg/s)" + delimeter + "Q (deg/s)" + delimeter + "R (deg/s)" + delimeter;  in OpenFile()
122 …outstream << "P dot (deg/s^2)" + delimeter + "Q dot (deg/s^2)" + delimeter + "R dot (deg/s^2)" + d…  in OpenFile()
123 …outstream << "P_{inertial} (deg/s)" + delimeter + "Q_{inertial} (deg/s)" + delimeter + "R_{inertia…  in OpenFile()
126     outstream << delimeter;  in OpenFile()
127     outstream << "q bar (psf)" + delimeter;  in OpenFile()
128     outstream << "Reynolds Number" + delimeter;  in OpenFile()
129     outstream << "V_{Total} (ft/s)" + delimeter;  in OpenFile()
130     outstream << "V_{Inertial} (ft/s)" + delimeter;  in OpenFile()
131     outstream << "UBody" + delimeter + "VBody" + delimeter + "WBody" + delimeter;  in OpenFile()
132     outstream << "UdotBody" + delimeter + "VdotBody" + delimeter + "WdotBody" + delimeter;  in OpenFile()
133     outstream << "UdotBody_i" + delimeter + "VdotBody_i" + delimeter + "WdotBody_i" + delimeter;  in OpenFile()
134     outstream << "BodyAccel_X" + delimeter + "BodyAccel_Y" + delimeter + "BodyAccel_Z" + delimeter;  in OpenFile()
135 …am << "Aero V_{X Body} (ft/s)" + delimeter + "Aero V_{Y Body} (ft/s)" + delimeter + "Aero V_{Z Bod…  in OpenFile()
136 … << "V_{X_{inertial}} (ft/s)" + delimeter + "V_{Y_{inertial}} (ft/s)" + delimeter + "V_{Z_{inertia…  in OpenFile()
137 …utstream << "V_{X_{ecef}} (ft/s)" + delimeter + "V_{Y_{ecef}} (ft/s)" + delimeter + "V_{Z_{ecef}} …  in OpenFile()
138     outstream << "V_{North} (ft/s)" + delimeter + "V_{East} (ft/s)" + delimeter + "V_{Down} (ft/s)";  in OpenFile()
141     outstream << delimeter;  in OpenFile()
142 …outstream << "F_{Drag} (lbs)" + delimeter + "F_{Side} (lbs)" + delimeter + "F_{Lift} (lbs)" + deli…  in OpenFile()
143     outstream << "L/D" + delimeter;  in OpenFile()
144 …outstream << "F_{Aero x} (lbs)" + delimeter + "F_{Aero y} (lbs)" + delimeter + "F_{Aero z} (lbs)" …  in OpenFile()
145 …outstream << "F_{Prop x} (lbs)" + delimeter + "F_{Prop y} (lbs)" + delimeter + "F_{Prop z} (lbs)" …  in OpenFile()
146 …outstream << "F_{Gear x} (lbs)" + delimeter + "F_{Gear y} (lbs)" + delimeter + "F_{Gear z} (lbs)" …  in OpenFile()
147 …outstream << "F_{Ext x} (lbs)" + delimeter + "F_{Ext y} (lbs)" + delimeter + "F_{Ext z} (lbs)" + d…  in OpenFile()
148 …utstream << "F_{Buoyant x} (lbs)" + delimeter + "F_{Buoyant y} (lbs)" + delimeter + "F_{Buoyant z}…  in OpenFile()
149 …outstream << "F_{Weight x} (lbs)" + delimeter + "F_{Weight y} (lbs)" + delimeter + "F_{Weight z} (…  in OpenFile()
150 …outstream << "F_{Total x} (lbs)" + delimeter + "F_{Total y} (lbs)" + delimeter + "F_{Total z} (lbs…  in OpenFile()
153     outstream << delimeter;  in OpenFile()
154 …outstream << "L_{Aero} (ft-lbs)" + delimeter + "M_{Aero} (ft-lbs)" + delimeter + "N_{Aero} (ft-lbs…  in OpenFile()
155 …ream << "L_{Aero MRC} (ft-lbs)" + delimeter + "M_{Aero MRC} (ft-lbs)" + delimeter + "N_{Aero MRC} …  in OpenFile()
156 …outstream << "L_{Prop} (ft-lbs)" + delimeter + "M_{Prop} (ft-lbs)" + delimeter + "N_{Prop} (ft-lbs…  in OpenFile()
157 …outstream << "L_{Gear} (ft-lbs)" + delimeter + "M_{Gear} (ft-lbs)" + delimeter + "N_{Gear} (ft-lbs…  in OpenFile()
158 …outstream << "L_{ext} (ft-lbs)" + delimeter + "M_{ext} (ft-lbs)" + delimeter + "N_{ext} (ft-lbs)" …  in OpenFile()
159 …stream << "L_{Buoyant} (ft-lbs)" + delimeter + "M_{Buoyant} (ft-lbs)" + delimeter + "N_{Buoyant} (…  in OpenFile()
160 …outstream << "L_{Total} (ft-lbs)" + delimeter + "M_{Total} (ft-lbs)" + delimeter + "N_{Total} (ft-…  in OpenFile()
163     outstream << delimeter;  in OpenFile()
164     outstream << "Rho (slugs/ft^3)" + delimeter;  in OpenFile()
165     outstream << "Absolute Viscosity" + delimeter;  in OpenFile()
166     outstream << "Kinematic Viscosity" + delimeter;  in OpenFile()
167     outstream << "Temperature (R)" + delimeter;  in OpenFile()
168     outstream << "P_{SL} (psf)" + delimeter;  in OpenFile()
169     outstream << "P_{Ambient} (psf)" + delimeter;  in OpenFile()
170     outstream << "Turbulence Magnitude (ft/sec)" + delimeter;  in OpenFile()
171     outstream << "Turbulence X Direction (deg)" + delimeter;  in OpenFile()
172 …tream << "Wind V_{North} (ft/s)" + delimeter + "Wind V_{East} (ft/s)" + delimeter + "Wind V_{Down}…  in OpenFile()
173 …outstream << "Roll Turbulence (deg/sec)" + delimeter + "Pitch Turbulence (deg/sec)" + delimeter + …  in OpenFile()
176     outstream << delimeter;  in OpenFile()
177     outstream << "I_{xx}" + delimeter;  in OpenFile()
178     outstream << "I_{xy}" + delimeter;  in OpenFile()
179     outstream << "I_{xz}" + delimeter;  in OpenFile()
180     outstream << "I_{yx}" + delimeter;  in OpenFile()
181     outstream << "I_{yy}" + delimeter;  in OpenFile()
182     outstream << "I_{yz}" + delimeter;  in OpenFile()
183     outstream << "I_{zx}" + delimeter;  in OpenFile()
184     outstream << "I_{zy}" + delimeter;  in OpenFile()
185     outstream << "I_{zz}" + delimeter;  in OpenFile()
186     outstream << "Mass" + delimeter;  in OpenFile()
187     outstream << "Weight" + delimeter;  in OpenFile()
188     outstream << "X_{cg}" + delimeter + "Y_{cg}" + delimeter + "Z_{cg}";  in OpenFile()
191     outstream << delimeter;  in OpenFile()
192     outstream << "Altitude ASL (ft)" + delimeter;  in OpenFile()
193     outstream << "Altitude AGL (ft)" + delimeter;  in OpenFile()
194     outstream << "Phi (deg)" + delimeter + "Theta (deg)" + delimeter + "Psi (deg)" + delimeter;  in OpenFile()
195 …tstream << "Q(1)_{LOCAL}" + delimeter + "Q(2)_{LOCAL}" + delimeter + "Q(3)_{LOCAL}" + delimeter + …  in OpenFile()
196 …outstream << "Q(1)_{ECEF}" + delimeter + "Q(2)_{ECEF}" + delimeter + "Q(3)_{ECEF}" + delimeter + "…  in OpenFile()
197 …outstream << "Q(1)_{ECI}" + delimeter + "Q(2)_{ECI}" + delimeter + "Q(3)_{ECI}" + delimeter + "Q(4…  in OpenFile()
198     outstream << "Alpha (deg)" + delimeter;  in OpenFile()
199     outstream << "Beta (deg)" + delimeter;  in OpenFile()
200     outstream << "Latitude (deg)" + delimeter;  in OpenFile()
201     outstream << "Latitude Geodetic (deg)" + delimeter;  in OpenFile()
202     outstream << "Longitude (deg)" + delimeter;  in OpenFile()
203 … outstream << "X_{ECI} (ft)" + delimeter + "Y_{ECI} (ft)" + delimeter + "Z_{ECI} (ft)" + delimeter;  in OpenFile()
204 …outstream << "X_{ECEF} (ft)" + delimeter + "Y_{ECEF} (ft)" + delimeter + "Z_{ECEF} (ft)" + delimet…  in OpenFile()
205     outstream << "Earth Position Angle (deg)" + delimeter;  in OpenFile()
206     outstream << "Distance AGL (ft)" + delimeter;  in OpenFile()
210     scratch = Aerodynamics->GetAeroFunctionStrings(delimeter);  in OpenFile()
211     if (scratch.length() != 0) outstream << delimeter << scratch;  in OpenFile()
214     scratch = FCS->GetComponentStrings(delimeter);  in OpenFile()
215     if (scratch.length() != 0) outstream << delimeter << scratch;  in OpenFile()
218     outstream << delimeter;  in OpenFile()
219     outstream << GroundReactions->GetGroundReactionStrings(delimeter);  in OpenFile()
222     outstream << delimeter;  in OpenFile()
223     outstream << Propulsion->GetPropulsionStrings(delimeter);  in OpenFile()
228       outstream << delimeter << OutputCaptions[i];  in OpenFile()
230       outstream << delimeter << OutputParameters[i]->GetFullyQualifiedName();  in OpenFile()
235       outstream << delimeter << PreFunctions[i]->GetName();  in OpenFile()
266     outstream << delimeter;  in Print()
267     outstream << FCS->GetDaCmd() << delimeter;  in Print()
268     outstream << FCS->GetDeCmd() << delimeter;  in Print()
269     outstream << FCS->GetDrCmd() << delimeter;  in Print()
270     outstream << FCS->GetDfCmd() << delimeter;  in Print()
271     outstream << FCS->GetDaLPos(ofDeg) << delimeter;  in Print()
272     outstream << FCS->GetDaRPos(ofDeg) << delimeter;  in Print()
273     outstream << FCS->GetDePos(ofDeg) << delimeter;  in Print()
274     outstream << FCS->GetDrPos(ofDeg) << delimeter;  in Print()
278     outstream << delimeter;  in Print()
279     outstream << (radtodeg*Propagate->GetPQR()).Dump(delimeter) << delimeter;  in Print()
280     outstream << (radtodeg*Accelerations->GetPQRdot()).Dump(delimeter) << delimeter;  in Print()
281     outstream << (radtodeg*Propagate->GetPQRi()).Dump(delimeter);  in Print()
284     outstream << delimeter;  in Print()
285     outstream << Auxiliary->Getqbar() << delimeter;  in Print()
286     outstream << Auxiliary->GetReynoldsNumber() << delimeter;  in Print()
287     outstream << setprecision(12) << Auxiliary->GetVt() << delimeter;  in Print()
288     outstream << Propagate->GetInertialVelocityMagnitude() << delimeter;  in Print()
289     outstream << setprecision(12) << Propagate->GetUVW().Dump(delimeter) << delimeter;  in Print()
290     outstream << setprecision(12) << Accelerations->GetUVWdot().Dump(delimeter) << delimeter;  in Print()
291     outstream << setprecision(12) << Accelerations->GetUVWidot().Dump(delimeter) << delimeter;  in Print()
292     outstream << setprecision(12) << Accelerations->GetBodyAccel().Dump(delimeter) << delimeter;  in Print()
293     outstream << Auxiliary->GetAeroUVW().Dump(delimeter) << delimeter;  in Print()
294     outstream << Propagate->GetInertialVelocity().Dump(delimeter) << delimeter;  in Print()
295     outstream << Propagate->GetECEFVelocity().Dump(delimeter) << delimeter;  in Print()
296     outstream << Propagate->GetVel().Dump(delimeter);  in Print()
300     outstream << delimeter;  in Print()
301     outstream << Aerodynamics->GetvFw().Dump(delimeter) << delimeter;  in Print()
302     outstream << Aerodynamics->GetLoD() << delimeter;  in Print()
303     outstream << Aerodynamics->GetForces().Dump(delimeter) << delimeter;  in Print()
304     outstream << Propulsion->GetForces().Dump(delimeter) << delimeter;  in Print()
305     outstream << Accelerations->GetGroundForces().Dump(delimeter) << delimeter;  in Print()
306     outstream << ExternalReactions->GetForces().Dump(delimeter) << delimeter;  in Print()
307     outstream << BuoyantForces->GetForces().Dump(delimeter) << delimeter;  in Print()
308     outstream << Accelerations->GetWeight().Dump(delimeter) << delimeter;  in Print()
309     outstream << Accelerations->GetForces().Dump(delimeter);  in Print()
312     outstream << delimeter;  in Print()
313     outstream << Aerodynamics->GetMoments().Dump(delimeter) << delimeter;  in Print()
314     outstream << Aerodynamics->GetMomentsMRC().Dump(delimeter) << delimeter;  in Print()
315     outstream << Propulsion->GetMoments().Dump(delimeter) << delimeter;  in Print()
316     outstream << Accelerations->GetGroundMoments().Dump(delimeter) << delimeter;  in Print()
317     outstream << ExternalReactions->GetMoments().Dump(delimeter) << delimeter;  in Print()
318     outstream << BuoyantForces->GetMoments().Dump(delimeter) << delimeter;  in Print()
319     outstream << Accelerations->GetMoments().Dump(delimeter);  in Print()
322     outstream << delimeter;  in Print()
323     outstream << Atmosphere->GetDensity() << delimeter;  in Print()
324     outstream << Atmosphere->GetAbsoluteViscosity() << delimeter;  in Print()
325     outstream << Atmosphere->GetKinematicViscosity() << delimeter;  in Print()
326     outstream << Atmosphere->GetTemperature() << delimeter;  in Print()
327     outstream << Atmosphere->GetPressureSL() << delimeter;  in Print()
328     outstream << Atmosphere->GetPressure() << delimeter;  in Print()
329     outstream << Winds->GetTurbMagnitude() << delimeter;  in Print()
330     outstream << Winds->GetTurbDirection() << delimeter;  in Print()
331     outstream << Winds->GetTotalWindNED().Dump(delimeter) << delimeter;  in Print()
332     outstream << (Winds->GetTurbPQR()*radtodeg).Dump(delimeter);  in Print()
335     outstream << delimeter;  in Print()
336     outstream << MassBalance->GetJ().Dump(delimeter) << delimeter;  in Print()
337     outstream << MassBalance->GetMass() << delimeter;  in Print()
338     outstream << MassBalance->GetWeight() << delimeter;  in Print()
339     outstream << MassBalance->GetXYZcg().Dump(delimeter);  in Print()
343     outstream << delimeter;  in Print()
344     outstream << Propagate->GetAltitudeASL() << delimeter;  in Print()
345     outstream << Propagate->GetDistanceAGL() << delimeter;  in Print()
346     outstream << (radtodeg*Propagate->GetEuler()).Dump(delimeter) << delimeter;  in Print()
347     outstream << Propagate->GetQuaternion().Dump(delimeter) << delimeter;  in Print()
349     outstream << Qec.Dump(delimeter) << delimeter;  in Print()
350     outstream << Propagate->GetQuaternionECI().Dump(delimeter) << delimeter;  in Print()
351     outstream << Auxiliary->Getalpha(inDegrees) << delimeter;  in Print()
352     outstream << Auxiliary->Getbeta(inDegrees) << delimeter;  in Print()
353     outstream << Propagate->GetLatitudeDeg() << delimeter;  in Print()
354     outstream << Propagate->GetGeodLatitudeDeg() << delimeter;  in Print()
355     outstream << Propagate->GetLongitudeDeg() << delimeter;  in Print()
357     outstream << ((FGColumnVector3)Propagate->GetInertialPosition()).Dump(delimeter) << delimeter;  in Print()
358     outstream << ((FGColumnVector3)Propagate->GetLocation()).Dump(delimeter) << delimeter;  in Print()
360     outstream << Propagate->GetEarthPositionAngleDeg() << delimeter;  in Print()
361     outstream << Propagate->GetDistanceAGL() << delimeter;  in Print()
366     scratch = Aerodynamics->GetAeroFunctionValues(delimeter);  in Print()
367     if (scratch.length() != 0) outstream << delimeter << scratch;  in Print()
370     scratch = FCS->GetComponentValues(delimeter);  in Print()
371     if (scratch.length() != 0) outstream << delimeter << scratch;  in Print()
374     outstream << delimeter;  in Print()
375     outstream << GroundReactions->GetGroundReactionValues(delimeter);  in Print()
378     outstream << delimeter;  in Print()
379     outstream << Propulsion->GetPropulsionValues(delimeter);  in Print()
384     outstream << delimeter << OutputParameters[i]->GetValue();  in Print()
387     outstream << delimeter << PreFunctions[i]->getDoubleValue();  in Print()