2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-05 21:26:01 +00:00
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Header: FGCoefficient.h
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Author: Jon Berndt
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Date started: 12/28/98
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------------- Copyright (C) 1999 Jon S. Berndt (jsb@hal-pc.org) -------------
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This program is free software; you can redistribute it and/or modify it under
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the terms of the GNU General Public License as published by the Free Software
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Foundation; either version 2 of the License, or (at your option) any later
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version.
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This program is distributed in the hope that it will be useful, but WITHOUT
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ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS
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FOR A PARTICULAR PURPOSE. See the GNU General Public License for more
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details.
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You should have received a copy of the GNU General Public License along with
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this program; if not, write to the Free Software Foundation, Inc., 59 Temple
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Place - Suite 330, Boston, MA 02111-1307, USA.
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Further information about the GNU General Public License can also be found on
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the world wide web at http://www.gnu.org.
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HISTORY
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--------------------------------------------------------------------------------
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12/28/98 JSB Created
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-05 21:26:01 +00:00
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SENTRY
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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1999-02-05 21:26:01 +00:00
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#ifndef FGCOEFFICIENT_H
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#define FGCOEFFICIENT_H
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2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-05 21:26:01 +00:00
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INCLUDES
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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Updates from the Jon and Tony show.
Tony submitted:
JSBsim:
Added trimming routine, it is longitudinal & in-air only at this point
Added support for taking wind & weather data from external source
Added support for flaps.
Added independently settable pitch trim
Added alphamin and max to config file, stall modeling and warning to
follow
c172.cfg:
Flaps!
Adjusted Cmo, model should be speed stable now
FG:
Hooked up Christian's weather code, should be using it soon.
Hooked up the trimming routine. Note that the X-15 will not trim.
This is not a model or trimming routine deficiency, just the
nature of the X-15
The trimming routine sets the pitch trim and and throttle at startup.
The throttle is set using Norman's code for the autothrottle so the
autothrottle is on by default. --notrim will turn it off.
Added --vc, --mach, and --notrim switches
(vc is airspeed in knots)
uBody, vBody, and wBody are still supported, last one entered
on the command line counts, i.e. you can set vc or mach or u,v,
and w but any combination will be ignored.
2000-05-16 21:35:11 +00:00
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1999-02-26 22:09:10 +00:00
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#ifdef FGFS
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2000-02-15 03:30:01 +00:00
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# include <simgear/compiler.h>
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1999-02-26 22:09:10 +00:00
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#endif
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1999-02-05 21:26:01 +00:00
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2000-10-02 23:07:30 +00:00
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#include <vector>
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Updates from the Jon and Tony show.
Tony submitted:
JSBsim:
Added trimming routine, it is longitudinal & in-air only at this point
Added support for taking wind & weather data from external source
Added support for flaps.
Added independently settable pitch trim
Added alphamin and max to config file, stall modeling and warning to
follow
c172.cfg:
Flaps!
Adjusted Cmo, model should be speed stable now
FG:
Hooked up Christian's weather code, should be using it soon.
Hooked up the trimming routine. Note that the X-15 will not trim.
This is not a model or trimming routine deficiency, just the
nature of the X-15
The trimming routine sets the pitch trim and and throttle at startup.
The throttle is set using Norman's code for the autothrottle so the
autothrottle is on by default. --notrim will turn it off.
Added --vc, --mach, and --notrim switches
(vc is airspeed in knots)
uBody, vBody, and wBody are still supported, last one entered
on the command line counts, i.e. you can set vc or mach or u,v,
and w but any combination will be ignored.
2000-05-16 21:35:11 +00:00
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#include <string>
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2000-04-24 23:49:06 +00:00
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#include "FGConfigFile.h"
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#include "FGDefs.h"
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1999-06-21 05:01:31 +00:00
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2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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DEFINITIONS
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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1999-05-08 03:19:08 +00:00
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2000-10-14 02:10:10 +00:00
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#define ID_COEFFICIENT "$Header"
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2000-11-03 23:02:47 +00:00
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using std::vector;
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-03-02 01:02:51 +00:00
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FORWARD DECLARATIONS
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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2000-10-02 23:07:30 +00:00
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1999-02-11 21:05:34 +00:00
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class FGFDMExec;
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class FGState;
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class FGAtmosphere;
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class FGFCS;
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class FGAircraft;
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class FGTranslation;
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class FGRotation;
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class FGPosition;
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class FGAuxiliary;
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class FGOutput;
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2000-11-03 23:02:47 +00:00
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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COMMENTS, REFERENCES, and NOTES [use "class documentation" below for API docs]
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-06-21 05:01:31 +00:00
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2000-11-03 23:02:47 +00:00
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Note that the coefficients need not be calculated each delta-t. This is
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something that may be fixed someday.
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1999-03-02 01:02:51 +00:00
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2000-11-03 23:02:47 +00:00
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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CLASS DOCUMENTATION
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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1999-03-02 01:02:51 +00:00
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2000-11-03 23:02:47 +00:00
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/** This class models the stability derivative coefficient lookup tables.
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Each coefficient for an axis is stored in that axes' vector of coefficients.
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Each FDM execution frame the Run() method of the [currently] FGAircraft model
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is called and the coefficient value is calculated.
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@author Jon S. Berndt
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@version $Id$
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@see -
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*/
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/*%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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CLASS DECLARATION
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%*/
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2000-10-02 23:07:30 +00:00
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1999-02-05 21:26:01 +00:00
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class FGCoefficient
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{
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2000-10-02 23:07:30 +00:00
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typedef vector <eParam> MultVec;
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1999-03-02 01:02:51 +00:00
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enum Type {UNKNOWN, VALUE, VECTOR, TABLE, EQUATION};
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2000-04-24 23:49:06 +00:00
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int numInstances;
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1999-02-26 22:09:10 +00:00
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string filename;
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string description;
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string name;
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string method;
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1999-02-05 21:26:01 +00:00
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float StaticValue;
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2000-10-02 23:07:30 +00:00
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float **Table;
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eParam LookupR, LookupC;
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MultVec multipliers;
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1999-02-05 21:26:01 +00:00
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int rows, columns;
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1999-03-02 01:02:51 +00:00
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Type type;
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1999-12-30 18:01:59 +00:00
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float SD; // Actual stability derivative (or other coefficient) value
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2000-11-14 20:31:58 +00:00
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float gain,bias;
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1999-02-05 21:26:01 +00:00
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1999-02-11 21:05:34 +00:00
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FGFDMExec* FDMExec;
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FGState* State;
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FGAtmosphere* Atmosphere;
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FGFCS* FCS;
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FGAircraft* Aircraft;
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FGTranslation* Translation;
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FGRotation* Rotation;
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FGPosition* Position;
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FGAuxiliary* Auxiliary;
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FGOutput* Output;
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2000-10-02 23:07:30 +00:00
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bool DeAllocate(void);
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bool Allocate(int, int);
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public:
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FGCoefficient(FGFDMExec*, FGConfigFile*);
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~FGCoefficient(void);
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float Value(float, float);
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float Value(float);
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float Value(void);
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float TotalValue(void);
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inline string Getname(void) {return name;}
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inline float GetSD(void) {return SD;}
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inline MultVec Getmultipliers(void) {return multipliers;}
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void DumpSD(void);
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2000-11-14 20:31:58 +00:00
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inline float GetGain(void) { return gain; }
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inline float GetBias(void) { return bias; }
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inline void SetGain(float tt) { gain = tt; }
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inline void SetBias(float tt) { bias = tt; }
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inline void ResetGB(void) { gain = 1.0; bias = 0.0; }
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2000-10-02 23:07:30 +00:00
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1999-02-05 21:26:01 +00:00
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};
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2000-11-03 23:02:47 +00:00
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//%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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1999-02-05 21:26:01 +00:00
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#endif
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