#include "FGModel.h"
#include "FGEngine.h"
#include "FGTank.h"
-#include "FGThruster.h"
#include "FGMatrix33.h"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
/** Propulsion management class.
The Propulsion class is the container for the entire propulsion system, which is
- comprised of engines, tanks, and "thrusters" (the device that transforms the
- engine power into a force that acts on the aircraft, such as a nozzle or
- propeller). Once the Propulsion class gets the config file, it reads in
- information which is specific to a type of engine. Then:
+ comprised of engines, and tanks. Once the Propulsion class gets the config file,
+ it reads in information which is specific to a type of engine. Then:
-# The appropriate engine type instance is created
- -# A thruster object is instantiated, and is linked to the engine
-# At least one tank object is created, and is linked to an engine.
- At Run time each engines Calculate() method is called to return the excess power
- generated during that iteration. The drag from the previous iteration is sub-
- tracted to give the excess power available for thrust this pass. That quantity
- is passed to the thrusters associated with a particular engine - perhaps with a
- scaling mechanism (gearing?) to allow the engine to give its associated thrust-
- ers specific distributed portions of the excess power.
+ At Run time each engines Calculate() method is called.
@author Jon S. Berndt
@version $Id$
@see
FGEngine
FGTank
- FGThruster
*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
/** Executes the propulsion model.
The initial plan for the FGPropulsion class calls for Run() to be executed,
- performing the following tasks:
- <ol>
- <li>Determine the drag - or power required - for the attached thrust effector
- for this engine so that any feedback to the engine can be performed. This
- is done by calling FGThruster::CalculatePReq()</li>
- <li>Given 1, above, calculate the power available from the engine. This is
- done by calling FGEngine::CalculatePAvail()</li>
- <li>Next, calculate the thrust output from the thruster model given the power
- available and the power required. This may also result in new performance
- numbers for the thruster in the case of the propeller, at least. This
- result is returned from a call to Calculate().</li></ol>
+ calculating the power available from the engine.
[Note: Should we be checking the Starved flag here?] */
bool Run(void);
- /** Loads the propulsion system (engine[s], tank[s], thruster[s]).
+ /** Loads the propulsion system (engine[s] and tank[s]).
Characteristics of the propulsion system are read in from the config file.
@param AC_cfg pointer to the config file instance that describes the
aircraft being modeled.
if (index <= Tanks.size()-1) return Tanks[index];
else return 0L; }
- /** Retrieves a thruster object pointer from the list of thrusters.
- @param index the thruster index within the vector container
- @return the address of the specific thruster, or zero if no such thruster is
- available */
- inline FGThruster* GetThruster(unsigned int index) {
- if (index <= Thrusters.size()-1) return Thrusters[index];
- else return 0L; }
-
/** Returns the number of fuel tanks currently actively supplying fuel */
inline int GetnumSelectedFuelTanks(void) const {return numSelectedFuelTanks;}
/** Returns the number of oxidizer tanks currently actively supplying oxidizer */
inline int GetnumSelectedOxiTanks(void) const {return numSelectedOxiTanks;}
- /** Loops the engines/thrusters until thrust output steady (used for trimming) */
+ /** Loops the engines until thrust output steady (used for trimming) */
bool GetSteadyState(void);
/** starts the engines in IC mode (dt=0). All engine-specific setup must
be done before calling this (i.e. magnetos, starter engage, etc.) */
bool ICEngineStart(void);
- string GetPropulsionStrings(void);
- string GetPropulsionValues(void);
+ string GetPropulsionStrings(string delimeter);
+ string GetPropulsionValues(string delimeter);
inline FGColumnVector3& GetForces(void) {return vForces; }
inline double GetForces(int n) const { return vForces(n);}
inline FGColumnVector3& GetMoments(void) {return vMoments;}
inline double GetMoments(int n) const {return vMoments(n);}
+ inline bool GetRefuel(void) {return refuel;}
+ inline void SetRefuel(bool setting) {refuel = setting;}
+ double Transfer(int source, int target, double amount);
+ void DoRefuel(double time_slice);
+
FGColumnVector3& GetTanksMoment(void);
double GetTanksWeight(void);
}
inline int GetActiveEngine(void);
+ inline bool GetFuelFreeze(void) {return fuel_freeze;}
void SetMagnetos(int setting);
void SetStarter(int setting);
void SetCutoff(int setting=0);
void SetActiveEngine(int engine);
+ void SetFuelFreeze(bool f);
FGMatrix33& CalculateTankInertias(void);
void bind();
vector <FGEngine*> Engines;
vector <FGTank*> Tanks;
vector <FGTank*>::iterator iTank;
- vector <FGThruster*> Thrusters;
unsigned int numSelectedFuelTanks;
unsigned int numSelectedOxiTanks;
unsigned int numFuelTanks;
unsigned int numOxiTanks;
unsigned int numEngines;
unsigned int numTanks;
- unsigned int numThrusters;
int ActiveEngine;
- double dt;
FGColumnVector3 vForces;
FGColumnVector3 vMoments;
FGColumnVector3 vTankXYZ;
FGColumnVector3 vXYZtank_arm;
FGMatrix33 tankJ;
+ bool refuel;
+ bool fuel_freeze;
+
void Debug(int from);
};
}
projects / flightgear.git / blobdiff