1 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
7 ------------- Copyright (C) 1999 Jon S. Berndt (jon@jsbsim.org) -------------
9 This program is free software; you can redistribute it and/or modify it under
10 the terms of the GNU Lesser General Public License as published by the Free Software
11 Foundation; either version 2 of the License, or (at your option) any later
14 This program is distributed in the hope that it will be useful, but WITHOUT
15 ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
16 FOR A PARTICULAR PURPOSE. See the GNU Lesser General Public License for more
19 You should have received a copy of the GNU Lesser General Public License along with
20 this program; if not, write to the Free Software Foundation, Inc., 59 Temple
21 Place - Suite 330, Boston, MA 02111-1307, USA.
23 Further information about the GNU Lesser General Public License can also be found on
24 the world wide web at http://www.gnu.org.
26 FUNCTIONAL DESCRIPTION
27 --------------------------------------------------------------------------------
29 Based on Flightgear code, which is based on LaRCSim. This class simulates
33 --------------------------------------------------------------------------------
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43 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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47 #include "FGJSBBase.h"
48 #include "math/FGColumnVector3.h"
51 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
53 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
55 #define ID_TANK "$Id$"
57 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
59 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
64 class FGPropertyManager;
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71 /** Models a fuel tank.
73 <h3>Fuel Temperature:</h3>
75 Fuel temperature is calculated using the following assumptions:
77 Fuel temperature will only be calculated for tanks which have an initial fuel
78 temperature specified in the configuration file.
80 The surface area of the tank is estimated from the capacity in pounds. It
81 is assumed that the tank is a wing tank with dimensions h by 4h by 10h. The
82 volume of the tank is then 40(h)(h)(h). The area of the upper or lower
83 surface is then 40(h)(h). The volume is also equal to the capacity divided
84 by 49.368 lbs/cu-ft, for jet fuel. The surface area of one side can then be
85 derived from the tank's capacity.
87 The heat capacity of jet fuel is assumed to be 900 Joules/lbm/K, and the
88 heat transfer factor of the tank is 1.115 Watts/sq-ft/K.
92 Fuel dumping is handled by the FGPropulsion class. A standpipe can be defined
93 here for each tank which sets the level of contents (in pounds) which is not dumpable.
94 Default standpipe level is zero, making all contents dumpable.
96 <h3>Fuel Transfer:</h3>
98 Fuel transfer is handled by the FGPropulsion class, however the contents of tanks
99 may be manipulated directly using the SetContents() function here, or via the property
100 tree at <tt>propulsion/tank[i]/contents-lbs</tt>, where i is the tank number (Tanks
101 are automatically numbered, starting at zero, in the order in which they are read in
102 the aircraft configuration file). The latter method allows one to use a system of FCS
103 components to control tank contents.
105 <h3>Configuration File Format:</h3>
108 <tank type="{FUEL | OXIDIZER}">
109 <grain_config type="{CYLINDRICAL | ENDBURNING}">
110 <length unit="{IN | FT | M}"> {number} </radius>
112 <location unit="{FT | M | IN}">
117 <drain_location unit="{FT | M | IN}">
122 <radius unit="{IN | FT | M}"> {number} </radius>
123 <capacity unit="{LBS | KG}"> {number} </capacity>
124 <contents unit="{LBS | KG}"> {number} </contents>
125 <temperature> {number} </temperature> <!-- must be degrees fahrenheit -->
126 <standpipe unit="{LBS | KG"}> {number} </standpipe>
127 <priority> {integer} </priority>
128 <density unit="{KG/L | LBS/GAL}"> {number} </density>
132 <h3>Definition of the tank configuration file parameters:</h3>
134 - \b type - One of FUEL or OXIDIZER. This is required.
135 - \b radius - Equivalent radius of tank for modeling slosh, defaults to inches.
136 - \b grain_config type - One of CYLINDRICAL or ENDBURNING.
137 - \b length - length of tank for modeling solid fuel propellant grain, defaults to inches.
138 - \b capacity - Capacity, defaults to pounds.
139 - \b contents - Initial contents, defaults to pounds.
140 - \b temperature - Initial temperature, defaults to degrees Fahrenheit.
141 - \b standpipe - Minimum contents to which tank can dump, defaults to pounds.
142 - \b priority - Establishes feed sequence of tank. "1" is the highest priority.
143 - \b density - Density of liquid tank contents.
146 - \b x - Location of tank on aircraft's x-axis, defaults to inches.
147 - \b y - Location of tank on aircraft's y-axis, defaults to inches.
148 - \b z - Location of tank on aircraft's z-axis, defaults to inches.
151 - \b x - Location of tank drain on aircraft's x-axis, defaults to inches.
152 - \b y - Location of tank drain on aircraft's y-axis, defaults to inches.
153 - \b z - Location of tank drain on aircraft's z-axis, defaults to inches.
155 <h3>Default values of the tank configuration file parameters:</h3>
157 - \b type - ttUNKNOWN (causes a load error in the propulsion configuration)
158 - \b location, \b drain_location - both optional, but a warning message will
159 be printed to the console if the location is not given
160 - \b x - 0.0 (both full and drained CG locations)
161 - \b y - 0.0 (both full and drained CG locations)
162 - \b z - 0.0 (both full and drained CG locations)
164 - \b capacity - 0.00001 (tank capacity must not be zero)
166 - \b temperature - -9999.0 (flag which indicates no temperature is set)
167 - \b standpipe - 0.0 (all contents may be dumped)
168 - \b priority - 1 (highest feed sequence priority)
171 @author Jon Berndt, Dave Culp
172 @see Akbar, Raza et al. "A Simple Analysis of Fuel Addition to the CWT of
173 747", California Institute of Technology, 1998,
174 http://www.galcit.caltech.edu/EDL/projects/JetA/reports/lumped.pdf
177 /*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
179 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
181 class FGTank : public FGJSBBase
185 The constructor reads in the defining parameters from a configuration file.
186 @param exec a pointer to the base FGFDMExec instance.
187 @param el a pointer to the Tank element.
188 @param tank_number the tank number (zero based).
190 FGTank(FGFDMExec* exec, Element* el, int tank_number);
194 /** Removes fuel from the tank.
195 This function removes fuel from a tank. If the tank empties, it is
197 @param used the amount of fuel used in lbs.
198 @return the remaining contents of the tank in lbs.
200 double Drain(double used);
202 /** Performs local, tanks-specific calculations, such as fuel temperature.
203 This function calculates the temperature of the fuel in the tank.
204 @param dt the time step for this model.
205 @return the current temperature in degrees Celsius.
207 double Calculate(double dt);
209 /** Retrieves the type of tank: Fuel or Oxidizer.
210 @return the tank type, 0 for undefined, 1 for fuel, and 2 for oxidizer.
212 int GetType(void) {return Type;}
214 /** Resets the tank parameters to the initial conditions */
215 void ResetToIC(void);
217 /** If the tank is set to supply fuel, this function returns true.
218 @return true if this tank is set to a non-zero priority.*/
219 bool GetSelected(void) {return Selected;}
221 /** Gets the tank fill level.
222 @return the fill level in percent, from 0 to 100.*/
223 double GetPctFull(void) {return PctFull;}
225 /** Gets the capacity of the tank.
226 @return the capacity of the tank in pounds. */
227 double GetCapacity(void) {return Capacity;}
229 /** Gets the capacity of the tank.
230 @return the capacity of the tank in gallons. */
231 double GetCapacityGallons(void) {return Capacity/Density;}
233 /** Gets the contents of the tank.
234 @return the contents of the tank in pounds. */
235 double GetContents(void) const {return Contents;}
237 /** Gets the contents of the tank.
238 @return the contents of the tank in gallons. */
239 double GetContentsGallons(void) const {return Contents/Density;}
241 /** Gets the temperature of the fuel.
242 The temperature of the fuel is calculated if an initial tempearture is
243 given in the configuration file.
244 @return the temperature of the fuel in degrees C IF an initial temperature
245 is given, otherwise 0.0 C is returned. */
246 double GetTemperature_degC(void) {return Temperature;}
248 /** Gets the temperature of the fuel.
249 The temperature of the fuel is calculated if an initial tempearture is
250 given in the configuration file.
251 @return the temperature of the fuel in degrees F IF an initial temperature
252 is given, otherwise 32 degrees F is returned. */
253 double GetTemperature(void) {return CelsiusToFahrenheit(Temperature);}
255 double GetIxx(void) {return Ixx;}
256 double GetIyy(void) {return Iyy;}
257 double GetIzz(void) {return Izz;}
259 double GetStandpipe(void) {return Standpipe;}
261 int GetPriority(void) const {return Priority;}
262 void SetPriority(int p) { Priority = p; Selected = p>0 ? true:false; }
264 const FGColumnVector3 GetXYZ(void);
265 const double GetXYZ(int idx);
267 double Fill(double amount);
268 void SetContents(double amount);
269 void SetContentsGallons(double gallons);
270 void SetTemperature(double temp) { Temperature = temp; }
271 void SetStandpipe(double amount) { Standpipe = amount; }
272 void SetSelected(bool sel) { sel==true ? SetPriority(1):SetPriority(0); }
274 enum TankType {ttUNKNOWN, ttFUEL, ttOXIDIZER};
275 enum GrainType {gtUNKNOWN, gtCYLINDRICAL, gtENDBURNING};
282 std::string strGType;
283 FGColumnVector3 vXYZ;
284 FGColumnVector3 vXYZ_drain;
295 double Contents, InitialContents;
297 double Temperature, InitialTemperature;
298 double Standpipe, InitialStandpipe;
300 int Priority, InitialPriority;
302 FGPropertyManager* PropertyManager;
303 void CalculateInertias(void);
304 void Debug(int from);
307 //%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%