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flightgear/src/FDM/JSBSim/FGFDMExec.h

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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
Header: FGFDMExec.h
Author: Jon Berndt
Date started: 11/17/98
file The header file for the JSBSim executive.
------------- Copyright (C) 1999 Jon S. Berndt (jon@jsbsim.org) -------------
This program is free software; you can redistribute it and/or modify it under
the terms of the GNU Lesser General Public License as published by the Free Software
Foundation; either version 2 of the License, or (at your option) any later
version.
This program is distributed in the hope that it will be useful, but WITHOUT
ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
FOR A PARTICULAR PURPOSE. See the GNU Lesser General Public License for more
details.
You should have received a copy of the GNU Lesser General Public License along with
this program; if not, write to the Free Software Foundation, Inc., 59 Temple
Place - Suite 330, Boston, MA 02111-1307, USA.
Further information about the GNU Lesser General Public License can also be found on
the world wide web at http://www.gnu.org.
HISTORY
--------------------------------------------------------------------------------
11/17/98 JSB Created
7/31/99 TP Added RunIC function that runs the sim so that every frame
begins with the IC values from the given FGInitialCondition
object and dt=0.
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
SENTRY
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#ifndef FGFDMEXEC_HEADER_H
#define FGFDMEXEC_HEADER_H
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
INCLUDES
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#include "models/FGModel.h"
#include "models/FGOutput.h"
#include "models/FGInput.h"
#include "initialization/FGTrim.h"
#include "initialization/FGInitialCondition.h"
#include "FGJSBBase.h"
#include "input_output/FGPropertyManager.h"
#include "input_output/FGGroundCallback.h"
#include "input_output/FGXMLFileRead.h"
#include "models/FGPropagate.h"
#include "math/FGColumnVector3.h"
#include <vector>
#include <string>
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
DEFINITIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
#define ID_FDMEXEC "$Id: FGFDMExec.h,v 1.54 2010/10/07 03:17:29 jberndt Exp $"
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
FORWARD DECLARATIONS
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
namespace JSBSim {
class FGScript;
class FGTrim;
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DOCUMENTATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
/** Encapsulates the JSBSim simulation executive.
This class is the executive class through which all other simulation classes
are instantiated, initialized, and run. When integrated with FlightGear (or
other flight simulator) this class is typically instantiated by an interface
class on the simulator side.
At the time of simulation initialization, the interface
class creates an instance of this executive class. The
executive is subsequently directed to load the chosen aircraft specification
file:
@code
fdmex = new FGFDMExec( <20> );
result = fdmex->LoadModel( <20> );
@endcode
When an aircraft model is loaded, the config file is parsed and for each of the
sections of the config file (propulsion, flight control, etc.) the
corresponding Load() method is called (e.g. FGFCS::Load()).
Subsequent to the creation of the executive and loading of the model,
initialization is performed. Initialization involves copying control inputs
into the appropriate JSBSim data storage locations, configuring it for the set
of user supplied initial conditions, and then copying state variables from
JSBSim. The state variables are used to drive the instrument displays and to
place the vehicle model in world space for visual rendering:
@code
copy_to_JSBsim(); // copy control inputs to JSBSim
fdmex->RunIC(); // loop JSBSim once w/o integrating
copy_from_JSBsim(); // update the bus
@endcode
Once initialization is complete, cyclic execution proceeds:
@code
copy_to_JSBsim(); // copy control inputs to JSBSim
fdmex->Run(); // execute JSBSim
copy_from_JSBsim(); // update the bus
@endcode
JSBSim can be used in a standalone mode by creating a compact stub program
that effectively performs the same progression of steps as outlined above for
the integrated version, but with two exceptions. First, the copy_to_JSBSim()
and copy_from_JSBSim() functions are not used because the control inputs are
handled directly by the scripting facilities and outputs are handled by the
output (data logging) class. Second, the name of a script file can be supplied
to the stub program. Scripting (see FGScript) provides a way to supply command
inputs to the simulation:
@code
FDMExec = new JSBSim::FGFDMExec();
FDMExec->LoadScript( ScriptName ); // the script loads the aircraft and ICs
result = FDMExec->Run();
while (result) { // cyclic execution
result = FDMExec->Run(); // execute JSBSim
}
@endcode
The standalone mode has been useful for verifying changes before committing
updates to the source code repository. It is also useful for running sets of
tests that reveal some aspects of simulated aircraft performance, such as
range, time-to-climb, takeoff distance, etc.
<h3>JSBSim Debugging Directives</h3>
This describes to any interested entity the debug level
requested by setting the JSBSIM_DEBUG environment variable.
The bitmasked value choices are as follows:
- <b>unset</b>: In this case (the default) JSBSim would only print
out the normally expected messages, essentially echoing
the config files as they are read. If the environment
variable is not set, debug_lvl is set to 1 internally
- <b>0</b>: This requests JSBSim not to output any messages
whatsoever
- <b>1</b>: This value explicity requests the normal JSBSim
startup messages
- <b>2</b>: This value asks for a message to be printed out when
a class is instantiated
- <b>4</b>: When this value is set, a message is displayed when a
FGModel object executes its Run() method
- <b>8</b>: When this value is set, various runtime state variables
are printed out periodically
- <b>16</b>: When set various parameters are sanity checked and
a message is printed out when they go out of bounds
<h3>Properties</h3>
@property simulator/do_trim (write only) Can be set to the integer equivalent to one of
tLongitudinal (0), tFull (1), tGround (2), tPullup (3),
tCustom (4), tTurn (5). Setting this to a legal value
(such as by a script) causes a trim to be performed. This
property actually maps toa function call of DoTrim().
@author Jon S. Berndt
@version $Revision: 1.54 $
*/
/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
CLASS DECLARATION
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
class FGFDMExec : public FGJSBBase, public FGXMLFileRead
{
struct childData {
FGFDMExec* exec;
string info;
FGColumnVector3 Loc;
FGColumnVector3 Orient;
bool mated;
bool internal;
childData(void) {
info = "";
Loc = FGColumnVector3(0,0,0);
Orient = FGColumnVector3(0,0,0);
mated = true;
internal = false;
}
void Run(void) {exec->Run();}
void AssignState(FGPropagate* source_prop) {
exec->GetPropagate()->SetVState(source_prop->GetVState());
}
~childData(void) {
delete exec;
}
};
public:
/// Default constructors
FGFDMExec(FGPropertyManager* root = 0);
FGFDMExec(FGPropertyManager* root, unsigned int* fdmctr);
/// Default destructor
~FGFDMExec();
/** This routine places a model into the runlist at the specified rate. The
"rate" is not really a clock rate. It represents how many calls to the
FGFDMExec::Run() method must be made before the model is executed. A
value of 1 means that the model will be executed for each call to the
exec's Run() method. A value of 5 means that the model will only be
executed every 5th call to the exec's Run() method. Use of a rate other than
one is at this time not recommended.
@param model A pointer to the model being scheduled.
@param rate The rate at which to execute the model as described above.
@return Currently returns 0 always. */
void Schedule(FGModel* model, int rate);
/** This function executes each scheduled model in succession.
@return true if successful, false if sim should be ended */
bool Run(void);
/** Initializes the sim from the initial condition object and executes
each scheduled model without integrating i.e. dt=0.
@return true if successful */
bool RunIC(void);
/** Sets the ground callback pointer.
@param gc A pointer to a ground callback object. */
void SetGroundCallback(FGGroundCallback* gc);
/** Loads an aircraft model.
@param AircraftPath path to the aircraft/ directory. For instance:
"aircraft". Under aircraft, then, would be directories for various
modeled aircraft such as C172/, x15/, etc.
@param EnginePath path to the directory under which engine config
files are kept, for instance "engine"
@param SystemsPath path to the directory under which systems config
files are kept, for instance "systems"
@param model the name of the aircraft model itself. This file will
be looked for in the directory specified in the AircraftPath variable,
and in turn under the directory with the same name as the model. For
instance: "aircraft/x15/x15.xml"
@param addModelToPath set to true to add the model name to the
AircraftPath, defaults to true
@return true if successful */
bool LoadModel(const string& AircraftPath, const string& EnginePath, const string& SystemsPath,
const string& model, bool addModelToPath = true);
/** Loads an aircraft model. The paths to the aircraft and engine
config file directories must be set prior to calling this. See
below.
@param model the name of the aircraft model itself. This file will
be looked for in the directory specified in the AircraftPath variable,
and in turn under the directory with the same name as the model. For
instance: "aircraft/x15/x15.xml"
@param addModelToPath set to true to add the model name to the
AircraftPath, defaults to true
@return true if successful*/
bool LoadModel(const string& model, bool addModelToPath = true);
/** Loads a script
@param Script the full path name and file name for the script to be loaded.
@return true if successfully loadsd; false otherwise. */
bool LoadScript(const string& Script, double deltaT);
/** Sets the path to the engine config file directories.
@param path path to the directory under which engine config
files are kept, for instance "engine" */
bool SetEnginePath(const string& path) { EnginePath = RootDir + path; return true; }
/** Sets the path to the aircraft config file directories.
@param path path to the aircraft directory. For instance:
"aircraft". Under aircraft, then, would be directories for various
modeled aircraft such as C172/, x15/, etc. */
bool SetAircraftPath(const string& path) { AircraftPath = RootDir + path; return true; }
/** Sets the path to the systems config file directories.
@param path path to the directory under which systems config
files are kept, for instance "systems" */
bool SetSystemsPath(const string& path) { SystemsPath = RootDir + path; return true; }
/// @name Top-level executive State and Model retrieval mechanism
//@{
/// Returns the FGAtmosphere pointer.
inline FGAtmosphere* GetAtmosphere(void) {return Atmosphere;}
/// Returns the FGFCS pointer.
inline FGFCS* GetFCS(void) {return FCS;}
/// Returns the FGPropulsion pointer.
inline FGPropulsion* GetPropulsion(void) {return Propulsion;}
/// Returns the FGAircraft pointer.
inline FGMassBalance* GetMassBalance(void) {return MassBalance;}
/// Returns the FGAerodynamics pointer
inline FGAerodynamics* GetAerodynamics(void){return Aerodynamics;}
/// Returns the FGInertial pointer.
inline FGInertial* GetInertial(void) {return Inertial;}
/// Returns the FGGroundReactions pointer.
inline FGGroundReactions* GetGroundReactions(void) {return GroundReactions;}
/// Returns the FGExternalReactions pointer.
inline FGExternalReactions* GetExternalReactions(void) {return ExternalReactions;}
/// Returns the FGBuoyantForces pointer.
inline FGBuoyantForces* GetBuoyantForces(void) {return BuoyantForces;}
/// Returns the FGAircraft pointer.
inline FGAircraft* GetAircraft(void) {return Aircraft;}
/// Returns the FGPropagate pointer.
inline FGPropagate* GetPropagate(void) {return Propagate;}
/// Returns the FGAuxiliary pointer.
inline FGAuxiliary* GetAuxiliary(void) {return Auxiliary;}
/// Returns the FGInput pointer.
inline FGInput* GetInput(void) {return Input;}
/// Returns the FGGroundCallback pointer.
inline FGGroundCallback* GetGroundCallback(void) {return GroundCallback;}
/// Retrieves the script object
inline FGScript* GetScript(void) {return Script;}
// Returns a pointer to the FGInitialCondition object
inline FGInitialCondition* GetIC(void) {return IC;}
// Returns a pointer to the FGTrim object
FGTrim* GetTrim(void);
//@}
/// Retrieves the engine path.
inline const string& GetEnginePath(void) {return EnginePath;}
/// Retrieves the aircraft path.
inline const string& GetAircraftPath(void) {return AircraftPath;}
/// Retrieves the systems path.
inline const string& GetSystemsPath(void) {return SystemsPath;}
/// Retrieves the full aircraft path name.
inline const string& GetFullAircraftPath(void) {return FullAircraftPath;}
/** Retrieves the value of a property.
@param property the name of the property
@result the value of the specified property */
inline double GetPropertyValue(const string& property) {return instance->GetDouble(property);}
/** Sets a property value.
@param property the property to be set
@param value the value to set the property to */
inline void SetPropertyValue(const string& property, double value) {
instance->SetDouble(property, value);
}
/// Returns the model name.
const string& GetModelName(void) { return modelName; }
/*
/// Returns the current time.
double GetSimTime(void);
/// Returns the current frame time (delta T).
double GetDeltaT(void);
*/
/// Returns a pointer to the property manager object.
FGPropertyManager* GetPropertyManager(void);
/// Returns a vector of strings representing the names of all loaded models (future)
vector <string> EnumerateFDMs(void);
/// Gets the number of child FDMs.
int GetFDMCount(void) {return (int)ChildFDMList.size();}
/// Gets a particular child FDM.
childData* GetChildFDM(int i) {return ChildFDMList[i];}
/// Marks this instance of the Exec object as a "child" object.
void SetChild(bool ch) {IsChild = ch;}
/** Sets the output (logging) mechanism for this run.
Calling this function passes the name of an output directives file to
the FGOutput object associated with this run. The call to this function
should be made prior to loading an aircraft model. This call results in an
FGOutput object being built as the first Output object in the FDMExec-managed
list of Output objects that may be created for an aircraft model. If this call
is made after an aircraft model is loaded, there is no effect. Any Output
objects added by the aircraft model itself (in an &lt;output> element) will be
added after this one. Care should be taken not to refer to the same file
name.
An output directives file contains an &lt;output> &lt;/output> element, within
which should be specified the parameters or parameter groups that should
be logged.
@param fname the filename of an output directives file.
*/
bool SetOutputDirectives(const string& fname);
/** Sets (or overrides) the output filename
@param fname the name of the file to output data to
@return true if successful, false if there is no output specified for the flight model */
bool SetOutputFileName(const string& fname) {
if (Outputs.size() > 0) Outputs[0]->SetOutputFileName(fname);
else return false;
return true;
}
/** Retrieves the current output filename.
@return the name of the output file for the first output specified by the flight model.
If none is specified, the empty string is returned. */
string GetOutputFileName(void) {
if (Outputs.size() > 0) return Outputs[0]->GetOutputFileName();
else return string("");
}
/** Executes trimming in the selected mode.
* @param mode Specifies how to trim:
* - tLongitudinal=0
* - tFull
* - tGround
* - tPullup
* - tCustom
* - tTurn
* - tNone */
void DoTrim(int mode);
// void DoTrimAnalysis(int mode);
/// Disables data logging to all outputs.
void DisableOutput(void);
/// Enables data logging to all outputs.
void EnableOutput(void);
/// Pauses execution by preventing time from incrementing.
void Hold(void) {holding = true;}
/// Resumes execution from a "Hold".
void Resume(void) {holding = false;}
/// Returns true if the simulation is Holding (i.e. simulation time is not moving).
bool Holding(void) {return holding;}
/// Resets the initial conditions object and prepares the simulation to run again.
void ResetToInitialConditions(void);
/// Sets the debug level.
void SetDebugLevel(int level) {debug_lvl = level;}
struct PropertyCatalogStructure {
/// Name of the property.
string base_string;
/// The node for the property.
FGPropertyManager *node;
};
/** Builds a catalog of properties.
* This function descends the property tree and creates a list (an STL vector)
* containing the name and node for all properties.
* @param pcs The "root" property catalog structure pointer. */
void BuildPropertyCatalog(struct PropertyCatalogStructure* pcs);
/** Retrieves property or properties matching the supplied string.
* A string is returned that contains a carriage return delimited list of all
* strings in the property catalog that matches the supplied check string.
* @param check The string to search for in the property catalog.
* @return the carriage-return-delimited string containing all matching strings
* in the catalog. */
string QueryPropertyCatalog(const string& check);
// Print the contents of the property catalog for the loaded aircraft.
void PrintPropertyCatalog(void);
vector<string>& GetPropertyCatalog(void) {return PropertyCatalog;}
/// Use the MSIS atmosphere model.
void UseAtmosphereMSIS(void);
/// Use the Mars atmosphere model. (Not operative yet.)
void UseAtmosphereMars(void);
void SetTrimStatus(bool status){ trim_status = status; }
bool GetTrimStatus(void) const { return trim_status; }
void SetTrimMode(int mode){ ta_mode = mode; }
int GetTrimMode(void) const { return ta_mode; }
/// Returns the cumulative simulation time in seconds.
double GetSimTime(void) const { return sim_time; }
/// Returns the simulation delta T.
double GetDeltaT(void) {return dT;}
/// Suspends the simulation and sets the delta T to zero.
void SuspendIntegration(void) {saved_dT = dT; dT = 0.0;}
/// Resumes the simulation by resetting delta T to the correct value.
void ResumeIntegration(void) {dT = saved_dT;}
/** Returns the simulation suspension state.
@return true if suspended, false if executing */
bool IntegrationSuspended(void) {return dT == 0.0;}
/** Sets the current sim time.
@param cur_time the current time
@return the current simulation time. */
double Setsim_time(double cur_time) {
sim_time = cur_time;
return sim_time;
}
/** Sets the integration time step for the simulation executive.
@param delta_t the time step in seconds. */
void Setdt(double delta_t) { dT = delta_t; }
/** Sets the root directory where JSBSim starts looking for its system directories.
@param rootDir the string containing the root directory. */
void SetRootDir(const string& rootDir) {RootDir = rootDir;}
/** Retrieves teh Root Directory.
@return the string representing the root (base) JSBSim directory. */
const string& GetRootDir(void) const {return RootDir;}
/** Increments the simulation time.
@return the new simulation time. */
double IncrTime(void) {
sim_time += dT;
return sim_time;
}
/** Retrieves the current debug level setting. */
int GetDebugLevel(void) const {return debug_lvl;};
private:
int Error;
unsigned int Frame;
unsigned int IdFDM;
unsigned short Terminate;
double dT;
double saved_dT;
double sim_time;
bool holding;
bool Constructing;
bool modelLoaded;
bool IsChild;
bool root_overload;
string modelName;
string AircraftPath;
string FullAircraftPath;
string EnginePath;
string SystemsPath;
string CFGVersion;
string Release;
string RootDir;
bool trim_status;
int ta_mode;
FGGroundCallback* GroundCallback;
FGAtmosphere* Atmosphere;
FGFCS* FCS;
FGPropulsion* Propulsion;
FGMassBalance* MassBalance;
FGAerodynamics* Aerodynamics;
FGInertial* Inertial;
FGGroundReactions* GroundReactions;
FGExternalReactions* ExternalReactions;
FGBuoyantForces* BuoyantForces;
FGAircraft* Aircraft;
FGPropagate* Propagate;
FGAuxiliary* Auxiliary;
FGInput* Input;
FGScript* Script;
FGInitialCondition* IC;
FGTrim* Trim;
FGPropertyManager* Root;
FGPropertyManager* instance;
// The FDM counter is used to give each child FDM an unique ID. The root FDM has the ID 0
unsigned int* FDMctr;
vector <string> PropertyCatalog;
vector <FGOutput*> Outputs;
vector <childData*> ChildFDMList;
vector <FGModel*> Models;
void Initialize();
bool ReadFileHeader(Element*);
bool ReadChild(Element*);
bool ReadPrologue(Element*);
void ResetToInitialConditions(int mode);
bool Allocate(void);
bool DeAllocate(void);
void Initialize(FGInitialCondition *FGIC);
void Debug(int from);
};
}
//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
#endif
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