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flightgear/src/FDM/UIUCModel/uiuc_aircraft.h

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UIUC flight model contribution. This is based on LaRCsim, but can read the aircraft parameters from a file. It still uses Tony's <crappy> (and I mean that in a constructive way) gear model. :-)
2000-03-22 22:01:33 +00:00
/**********************************************************************
FILENAME: uiuc_aircraft.h
----------------------------------------------------------------------
DESCRIPTION: creates maps for all keywords and variables expected in
aircraft input file, includes all parameters that
define the aircraft for use in the uiuc aircraft models.
----------------------------------------------------------------------
STATUS: alpha version
----------------------------------------------------------------------
REFERENCES:
----------------------------------------------------------------------
HISTORY: 01/26/2000 initial release
02/10/2000 (JS) changed aeroData to aeroParts (etc.)
added Twin Otter 2.5 equation variables
added Dx_cg (etc.) to init & record maps
added controlsMixer to top level map
02/18/2000 (JS) added variables needed for 1D file
reading of CL and CD as functions of alpha
02/29/2000 (JS) added variables needed for 2D file
reading of CL, CD, and Cm as functions of
alpha and delta_e; of CY and Cn as function
of alpha and delta_r; and of Cl and Cn as
functions of alpha and delta_a
03/02/2000 (JS) added record features for 1D and 2D
interpolations
----------------------------------------------------------------------
AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
Jeff Scott <jscott@mail.com>
----------------------------------------------------------------------
VARIABLES:
----------------------------------------------------------------------
INPUTS: none
----------------------------------------------------------------------
OUTPUTS: none
----------------------------------------------------------------------
CALLED BY: uiuc_1DdataFileReader.cpp
uiuc_2DdataFileReader.cpp
uiuc_aerodeflections.cpp
uiuc_coefficients.cpp
uiuc_engine.cpp
uiuc_initializemaps.cpp
uiuc_menu.cpp
uiuc_recorder.cpp
----------------------------------------------------------------------
CALLS TO: none
----------------------------------------------------------------------
COPYRIGHT: (C) 2000 by Michael Selig
This program is free software; you can redistribute it and/or
modify it under the terms of the GNU General Public License
as published by the Free Software Foundation.
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 General Public License for more details.
You should have received a copy of the GNU 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 or view http://www.gnu.org/copyleft/gpl.html.
**********************************************************************/
#ifndef _AIRCRAFT_H_
#define _AIRCRAFT_H_
MacOS build updates.
2000-04-27 21:57:08 +00:00
#include <simgear/compiler.h>
UIUC flight model contribution. This is based on LaRCsim, but can read the aircraft parameters from a file. It still uses Tony's <crappy> (and I mean that in a constructive way) gear model. :-)
2000-03-22 22:01:33 +00:00
#include <map>
#include <iostream>
#include "uiuc_parsefile.h"
MacOS build updates.
2000-04-27 21:57:08 +00:00
FG_USING_STD(map);
FG_USING_STD(iostream);
MSVC5 Compatibility tweaks.
2000-05-24 04:27:28 +00:00
#if defined ( MACOS ) || defined ( _MSC_VER )
MacOS build updates.
2000-04-27 21:57:08 +00:00
FG_USING_STD(ofstream);
#endif
UIUC flight model contribution. This is based on LaRCsim, but can read the aircraft parameters from a file. It still uses Tony's <crappy> (and I mean that in a constructive way) gear model. :-)
2000-03-22 22:01:33 +00:00
typedef stack :: iterator LIST;
/* Add more keywords here if required*/
enum {init_flag = 1000, geometry_flag, controlSurface_flag, controlsMixer_flag,
mass_flag, engine_flag, CD_flag, CL_flag, Cm_flag, CY_flag, Cl_flag,
Cn_flag, gear_flag, ice_flag, record_flag};
// init ======= Initial values for equation of motion
enum {Dx_pilot_flag = 2000, Dy_pilot_flag, Dz_pilot_flag,
Dx_cg_flag, Dy_cg_flag, Dz_cg_flag,
V_north_flag, V_east_flag, V_down_flag,
P_body_flag, Q_body_flag, R_body_flag,
Phi_flag, Theta_flag, Psi_flag};
// geometry === Aircraft-specific geometric quantities
enum {bw_flag = 3000, cbar_flag, Sw_flag};
// controlSurface = Control surface deflections and properties
enum {de_flag = 4000, da_flag, dr_flag};
// controlsMixer == Controls mixer
enum {nomix_flag = 14000};
//mass ======== Aircraft-specific mass properties
enum {Mass_flag = 5000, I_xx_flag, I_yy_flag, I_zz_flag, I_xz_flag};
// engine ===== Propulsion data
enum {simpleSingle_flag = 6000, c172_flag};
// CD ========= Aerodynamic x-force quantities (longitudinal)
enum {CDo_flag = 7000, CDK_flag, CD_a_flag, CD_de_flag, CDfa_flag, CDfade_flag};
// CL ========= Aerodynamic z-force quantities (longitudinal)
enum {CLo_flag = 8000, CL_a_flag, CL_adot_flag, CL_q_flag, CL_de_flag, CLfa_flag, CLfade_flag};
// Cm ========= Aerodynamic m-moment quantities (longitudinal)
enum {Cmo_flag = 9000, Cm_a_flag, Cm_adot_flag, Cm_q_flag, Cm_de_flag, Cmfade_flag};
// CY ========= Aerodynamic y-force quantities (lateral)
enum {CYo_flag = 10000, CY_beta_flag, CY_p_flag, CY_r_flag, CY_da_flag, CY_dr_flag,
CYfada_flag, CYfbetadr_flag};
// Cl ========= Aerodynamic l-moment quantities (lateral)
enum {Clo_flag = 11000, Cl_beta_flag, Cl_betafCL_flag, Cl_p_flag, Cl_r_flag, Cl_rfCL_flag,
Cl_da_flag, Cl_dr_flag, Clfada_flag, Clfbetadr_flag};
// Cn ========= Aerodynamic n-moment quantities (lateral)
enum {Cno_flag = 12000, Cn_beta_flag, Cn_betafCL_flag, Cn_p_flag, Cn_pfCL_flag, Cn_r_flag,
Cn_rfCL_flag, Cn_da_flag, Cn_dr_flag, Cn_drfCL_flag, Cnfada_flag, Cnfbetadr_flag};
// gear ======= Landing gear model quantities
// ice ======== Ice model quantities
enum {iceTime_flag = 15000, transientTime_flag, eta_final_flag,
kCDo_flag, kCDK_flag, kCD_a_flag, kCD_de_flag,
kCLo_flag, kCL_a_flag, kCL_adot_flag, kCL_q_flag, kCL_de_flag,
kCmo_flag, kCm_a_flag, kCm_adot_flag, kCm_q_flag, kCm_de_flag,
kCYo_flag, kCY_beta_flag, kCY_p_flag, kCY_r_flag, kCY_da_flag, kCY_dr_flag,
kClo_flag, kCl_beta_flag, kCl_p_flag, kCl_r_flag, kCl_da_flag, kCl_dr_flag,
kCno_flag, kCn_beta_flag, kCn_p_flag, kCn_r_flag, kCn_da_flag, kCn_dr_flag};
// record ===== Record desired quantites to file
enum {Dx_pilot_record = 13000, Dy_pilot_record, Dz_pilot_record,
Dx_cg_record, Dy_cg_record, Dz_cg_record,
V_north_record, V_east_record, V_down_record,
V_rel_wind_record, Dynamic_pressure_record,
Alpha_record, Alpha_dot_record, Beta_record, Beta_dot_record, Gamma_record,
P_body_record, Q_body_record, R_body_record,
Phi_record, Theta_record, Psi_record, Theta_dot_record,
density_record, Mass_record, Simtime_record, dt_record,
elevator_record, aileron_record, rudder_record,
CD_record, CDfaI_record, CDfadeI_record,
CL_record, CLfaI_record, CLfadeI_record,
Cm_record, CmfadeI_record,
CY_record, CYfadaI_record, CYfbetadrI_record,
Cl_record, ClfadaI_record, ClfbetadrI_record,
Cn_record, CnfadaI_record, CnfbetadrI_record,
F_X_wind_record, F_Y_wind_record, F_Z_wind_record,
F_X_aero_record, F_Y_aero_record, F_Z_aero_record,
F_X_engine_record, F_Y_engine_record, F_Z_engine_record,
F_X_gear_record, F_Y_gear_record, F_Z_gear_record,
F_X_record, F_Y_record, F_Z_record,
M_l_aero_record, M_m_aero_record, M_n_aero_record,
M_l_engine_record, M_m_engine_record, M_n_engine_record,
M_l_gear_record, M_m_gear_record, M_n_gear_record,
M_l_rp_record, M_m_rp_record, M_n_rp_record};
typedef struct
{
// ParseFile stuff [] Bipin to add more comments
ParseFile *airplane;
#define airplane aircraft_->airplane
ParseFile *initParts;
#define initParts aircraft_->initParts
ParseFile *geometryParts;
#define geometryParts aircraft_->geometryParts
ParseFile *massParts;
#define massParts aircraft_->massParts
ParseFile *aeroParts;
#define aeroParts aircraft_->aeroParts
ParseFile *engineParts;
#define engineParts aircraft_->engineParts
ParseFile *gearParts;
#define gearParts aircraft_->gearParts
ParseFile *recordParts;
#define recordParts aircraft_->recordParts
/*= Keywords (token1) ===========================================*/
map <string,int> Keyword_map;
#define Keyword_map aircraft_->Keyword_map
double CL;
double CD;
double Cm;
double CY;
double Cl;
double Cn;
#define CL aircraft_->CL
#define CD aircraft_->CD
#define Cm aircraft_->Cm
#define CY aircraft_->CY
#define Cl aircraft_->Cl
#define Cn aircraft_->Cn
/*========================================*/
/* Variables (token2) - 14 groups (000210)*/
/*========================================*/
/* Variables (token2) ===========================================*/
/* init ========== Initial values for equations of motion =======*/
map <string,int> init_map;
#define init_map aircraft_->init_map
/* Variables (token2) ===========================================*/
/* geometry ====== Aircraft-specific geometric quantities =======*/
map <string,int> geometry_map;
#define geometry_map aircraft_->geometry_map
double bw;
double cbar;
double Sw;
#define bw aircraft_->bw
#define cbar aircraft_->cbar
#define Sw aircraft_->Sw
/* Variables (token2) ===========================================*/
/* controlSurface Control surface deflections and properties ===*/
map <string,int> controlSurface_map;
#define controlSurface_map aircraft_->controlSurface_map
double demax;
double demin;
double damax;
double damin;
double drmax;
double drmin;
#define demax aircraft_->demax
#define demin aircraft_->demin
#define damax aircraft_->damax
#define damin aircraft_->damin
#define drmax aircraft_->drmax
#define drmin aircraft_->drmin
double aileron;
double elevator;
double rudder;
#define aileron aircraft_->aileron
#define elevator aircraft_->elevator
#define rudder aircraft_->rudder
/* Variables (token2) ===========================================*/
/* controlsMixer = Control mixer ================================*/
map <string,int> controlsMixer_map;
#define controlsMixer_map aircraft_->controlsMixer_map
double nomix;
#define nomix aircraft_->nomix
/* Variables (token2) ===========================================*/
/* mass =========== Aircraft-specific mass properties ===========*/
map <string,int> mass_map;
#define mass_map aircraft_->mass_map
/* Variables (token2) ===========================================*/
/* engine ======== Propulsion data ==============================*/
map <string,int> engine_map;
#define engine_map aircraft_->engine_map
double simpleSingleMaxThrust;
#define simpleSingleMaxThrust aircraft_->simpleSingleMaxThrust
/* Variables (token2) ===========================================*/
/* CD ============ Aerodynamic x-force quantities (longitudinal) */
map <string,int> CD_map;
#define CD_map aircraft_->CD_map
double CDo;
double CDK;
double CD_a;
double CD_de;
#define CDo aircraft_->CDo
#define CDK aircraft_->CDK
#define CD_a aircraft_->CD_a
#define CD_de aircraft_->CD_de
string CDfa;
int CDfaData;
double CDfa_aArray[100];
double CDfa_CDArray[100];
int CDfa_nAlpha;
double CDfaI;
#define CDfa aircraft_->CDfa
#define CDfaData aircraft_->CDfaData
#define CDfa_aArray aircraft_->CDfa_aArray
#define CDfa_CDArray aircraft_->CDfa_CDArray
#define CDfa_nAlpha aircraft_->CDfa_nAlpha
#define CDfaI aircraft_->CDfaI
string CDfade;
int CDfadeData;
double CDfade_aArray[100][100];
double CDfade_deArray[100];
double CDfade_CDArray[100][100];
int CDfade_nAlphaArray[100];
int CDfade_nde;
double CDfadeI;
#define CDfade aircraft_->CDfade
#define CDfadeData aircraft_->CDfadeData
#define CDfade_aArray aircraft_->CDfade_aArray
#define CDfade_deArray aircraft_->CDfade_deArray
#define CDfade_CDArray aircraft_->CDfade_CDArray
#define CDfade_nAlphaArray aircraft_->CDfade_nAlphaArray
#define CDfade_nde aircraft_->CDfade_nde
#define CDfadeI aircraft_->CDfadeI
/* Variables (token2) ===========================================*/
/* CL ============ Aerodynamic z-force quantities (longitudinal) */
map <string,int> CL_map;
#define CL_map aircraft_->CL_map
double CLo;
double CL_a;
double CL_adot;
double CL_q;
double CL_de;
#define CLo aircraft_->CLo
#define CL_a aircraft_->CL_a
#define CL_adot aircraft_->CL_adot
#define CL_q aircraft_->CL_q
#define CL_de aircraft_->CL_de
string CLfa;
int CLfaData;
double CLfa_aArray[100];
double CLfa_CLArray[100];
int CLfa_nAlpha;
double CLfaI;
#define CLfa aircraft_->CLfa
#define CLfaData aircraft_->CLfaData
#define CLfa_aArray aircraft_->CLfa_aArray
#define CLfa_CLArray aircraft_->CLfa_CLArray
#define CLfa_nAlpha aircraft_->CLfa_nAlpha
#define CLfaI aircraft_->CLfaI
string CLfade;
int CLfadeData;
double CLfade_aArray[100][100];
double CLfade_deArray[100];
double CLfade_CLArray[100][100];
int CLfade_nAlphaArray[100];
int CLfade_nde;
double CLfadeI;
#define CLfade aircraft_->CLfade
#define CLfadeData aircraft_->CLfadeData
#define CLfade_aArray aircraft_->CLfade_aArray
#define CLfade_deArray aircraft_->CLfade_deArray
#define CLfade_CLArray aircraft_->CLfade_CLArray
#define CLfade_nAlphaArray aircraft_->CLfade_nAlphaArray
#define CLfade_nde aircraft_->CLfade_nde
#define CLfadeI aircraft_->CLfadeI
/* Variables (token2) ===========================================*/
/* Cm ============ Aerodynamic m-moment quantities (longitudinal) */
map <string,int> Cm_map;
#define Cm_map aircraft_->Cm_map
double Cmo;
double Cm_a;
double Cm_adot;
double Cm_q;
double Cm_de;
#define Cmo aircraft_->Cmo
#define Cm_a aircraft_->Cm_a
#define Cm_adot aircraft_->Cm_adot
#define Cm_q aircraft_->Cm_q
#define Cm_de aircraft_->Cm_de
string Cmfade;
int CmfadeData;
double Cmfade_aArray[100][100];
double Cmfade_deArray[100];
double Cmfade_CmArray[100][100];
int Cmfade_nAlphaArray[100];
int Cmfade_nde;
double CmfadeI;
#define Cmfade aircraft_->Cmfade
#define CmfadeData aircraft_->CmfadeData
#define Cmfade_aArray aircraft_->Cmfade_aArray
#define Cmfade_deArray aircraft_->Cmfade_deArray
#define Cmfade_CmArray aircraft_->Cmfade_CmArray
#define Cmfade_nAlphaArray aircraft_->Cmfade_nAlphaArray
#define Cmfade_nde aircraft_->Cmfade_nde
#define CmfadeI aircraft_->CmfadeI
/* Variables (token2) ===========================================*/
/* CY ============ Aerodynamic y-force quantities (lateral) =====*/
map <string,int> CY_map;
#define CY_map aircraft_->CY_map
double CYo;
double CY_beta;
double CY_p;
double CY_r;
double CY_da;
double CY_dr;
#define CYo aircraft_->CYo
#define CY_beta aircraft_->CY_beta
#define CY_p aircraft_->CY_p
#define CY_r aircraft_->CY_r
#define CY_da aircraft_->CY_da
#define CY_dr aircraft_->CY_dr
string CYfada;
int CYfadaData;
double CYfada_aArray[100][100];
double CYfada_daArray[100];
double CYfada_CYArray[100][100];
int CYfada_nAlphaArray[100];
int CYfada_nda;
double CYfadaI;
#define CYfada aircraft_->CYfada
#define CYfadaData aircraft_->CYfadaData
#define CYfada_aArray aircraft_->CYfada_aArray
#define CYfada_daArray aircraft_->CYfada_daArray
#define CYfada_CYArray aircraft_->CYfada_CYArray
#define CYfada_nAlphaArray aircraft_->CYfada_nAlphaArray
#define CYfada_nda aircraft_->CYfada_nda
#define CYfadaI aircraft_->CYfadaI
string CYfbetadr;
int CYfbetadrData;
double CYfbetadr_betaArray[100][100];
double CYfbetadr_drArray[100];
double CYfbetadr_CYArray[100][100];
int CYfbetadr_nBetaArray[100];
int CYfbetadr_ndr;
double CYfbetadrI;
#define CYfbetadr aircraft_->CYfbetadr
#define CYfbetadrData aircraft_->CYfbetadrData
#define CYfbetadr_betaArray aircraft_->CYfbetadr_betaArray
#define CYfbetadr_drArray aircraft_->CYfbetadr_drArray
#define CYfbetadr_CYArray aircraft_->CYfbetadr_CYArray
#define CYfbetadr_nBetaArray aircraft_->CYfbetadr_nBetaArray
#define CYfbetadr_ndr aircraft_->CYfbetadr_ndr
#define CYfbetadrI aircraft_->CYfbetadrI
/* Variables (token2) ===========================================*/
/* Cl ============ Aerodynamic l-moment quantities (lateral) ====*/
map <string,int> Cl_map;
#define Cl_map aircraft_->Cl_map
double Clo;
double Cl_beta;
double Cl_betafCL;
double Cl_p;
double Cl_r;
double Cl_rfCL;
double Cl_da;
double Cl_dr;
#define Clo aircraft_->Clo
#define Cl_beta aircraft_->Cl_beta
#define Cl_betafCL aircraft_->Cl_betafCL
#define Cl_p aircraft_->Cl_p
#define Cl_r aircraft_->Cl_r
#define Cl_rfCL aircraft_->Cl_rfCL
#define Cl_da aircraft_->Cl_da
#define Cl_dr aircraft_->Cl_dr
string Clfada;
int ClfadaData;
double Clfada_aArray[100][100];
double Clfada_daArray[100];
double Clfada_ClArray[100][100];
int Clfada_nAlphaArray[100];
int Clfada_nda;
double ClfadaI;
#define Clfada aircraft_->Clfada
#define ClfadaData aircraft_->ClfadaData
#define Clfada_aArray aircraft_->Clfada_aArray
#define Clfada_daArray aircraft_->Clfada_daArray
#define Clfada_ClArray aircraft_->Clfada_ClArray
#define Clfada_nAlphaArray aircraft_->Clfada_nAlphaArray
#define Clfada_nda aircraft_->Clfada_nda
#define ClfadaI aircraft_->ClfadaI
string Clfbetadr;
int ClfbetadrData;
double Clfbetadr_betaArray[100][100];
double Clfbetadr_drArray[100];
double Clfbetadr_ClArray[100][100];
int Clfbetadr_nBetaArray[100];
int Clfbetadr_ndr;
double ClfbetadrI;
#define Clfbetadr aircraft_->Clfbetadr
#define ClfbetadrData aircraft_->ClfbetadrData
#define Clfbetadr_betaArray aircraft_->Clfbetadr_betaArray
#define Clfbetadr_drArray aircraft_->Clfbetadr_drArray
#define Clfbetadr_ClArray aircraft_->Clfbetadr_ClArray
#define Clfbetadr_nBetaArray aircraft_->Clfbetadr_nBetaArray
#define Clfbetadr_ndr aircraft_->Clfbetadr_ndr
#define ClfbetadrI aircraft_->ClfbetadrI
/* Variables (token2) ===========================================*/
/* Cn ============ Aerodynamic n-moment quantities (lateral) ====*/
map <string,int> Cn_map;
#define Cn_map aircraft_->Cn_map
double Cno;
double Cn_beta;
double Cn_p;
double Cn_r;
double Cn_da;
double Cn_dr;
#define Cno aircraft_->Cno
#define Cn_beta aircraft_->Cn_beta
#define Cn_p aircraft_->Cn_p
#define Cn_r aircraft_->Cn_r
#define Cn_da aircraft_->Cn_da
#define Cn_dr aircraft_->Cn_dr
string Cnfada;
int CnfadaData;
double Cnfada_aArray[100][100];
double Cnfada_daArray[100];
double Cnfada_CnArray[100][100];
int Cnfada_nAlphaArray[100];
int Cnfada_nda;
double CnfadaI;
#define Cnfada aircraft_->Cnfada
#define CnfadaData aircraft_->CnfadaData
#define Cnfada_aArray aircraft_->Cnfada_aArray
#define Cnfada_daArray aircraft_->Cnfada_daArray
#define Cnfada_CnArray aircraft_->Cnfada_CnArray
#define Cnfada_nAlphaArray aircraft_->Cnfada_nAlphaArray
#define Cnfada_nda aircraft_->Cnfada_nda
#define CnfadaI aircraft_->CnfadaI
string Cnfbetadr;
int CnfbetadrData;
double Cnfbetadr_betaArray[100][100];
double Cnfbetadr_drArray[100];
double Cnfbetadr_CnArray[100][100];
int Cnfbetadr_nBetaArray[100];
int Cnfbetadr_ndr;
double CnfbetadrI;
#define Cnfbetadr aircraft_->Cnfbetadr
#define CnfbetadrData aircraft_->CnfbetadrData
#define Cnfbetadr_betaArray aircraft_->Cnfbetadr_betaArray
#define Cnfbetadr_drArray aircraft_->Cnfbetadr_drArray
#define Cnfbetadr_CnArray aircraft_->Cnfbetadr_CnArray
#define Cnfbetadr_nBetaArray aircraft_->Cnfbetadr_nBetaArray
#define Cnfbetadr_ndr aircraft_->Cnfbetadr_ndr
#define CnfbetadrI aircraft_->CnfbetadrI
/* Variables (token2) ===========================================*/
/* gear ========== Landing gear model quantities ================*/
map <string,int> gear_map;
#define gear_map aircraft_->gear_map
/* Variables (token2) ===========================================*/
/* ice =========== Ice model quantities ======================== */
map <string,int> ice_map;
#define ice_map aircraft_->ice_map
double iceTime;
double transientTime;
double eta_final;
double eta;
#define iceTime aircraft_->iceTime
#define transientTime aircraft_->transientTime
#define eta_final aircraft_->eta_final
#define eta aircraft_->eta
double kCDo;
double kCDK;
double kCD_a;
double kCD_de;
double CDo_clean;
double CDK_clean;
double CD_a_clean;
double CD_de_clean;
#define kCDo aircraft_->kCDo
#define kCDK aircraft_->kCDK
#define kCD_a aircraft_->kCD_a
#define kCD_de aircraft_->kCD_de
#define CDo_clean aircraft_->CDo_clean
#define CDK_clean aircraft_->CDK_clean
#define CD_a_clean aircraft_->CD_a_clean
#define CD_de_clean aircraft_->CD_de_clean
double kCLo;
double kCL_a;
double kCL_adot;
double kCL_q;
double kCL_de;
double CLo_clean;
double CL_a_clean;
double CL_adot_clean;
double CL_q_clean;
double CL_de_clean;
#define kCLo aircraft_->kCLo
#define kCL_a aircraft_->kCL_a
#define kCL_adot aircraft_->kCL_adot
#define kCL_q aircraft_->kCL_q
#define kCL_de aircraft_->kCL_de
#define CLo_clean aircraft_->CLo_clean
#define CL_a_clean aircraft_->CL_a_clean
#define CL_adot_clean aircraft_->CL_adot_clean
#define CL_q_clean aircraft_->CL_q_clean
#define CL_de_clean aircraft_->CL_de_clean
double kCmo;
double kCm_a;
double kCm_adot;
double kCm_q;
double kCm_de;
double Cmo_clean;
double Cm_a_clean;
double Cm_adot_clean;
double Cm_q_clean;
double Cm_de_clean;
#define kCmo aircraft_->kCmo
#define kCm_a aircraft_->kCm_a
#define kCm_adot aircraft_->kCm_adot
#define kCm_q aircraft_->kCm_q
#define kCm_de aircraft_->kCm_de
#define Cmo_clean aircraft_->Cmo_clean
#define Cm_a_clean aircraft_->Cm_a_clean
#define Cm_adot_clean aircraft_->Cm_adot_clean
#define Cm_q_clean aircraft_->Cm_q_clean
#define Cm_de_clean aircraft_->Cm_de_clean
double kCYo;
double kCY_beta;
double kCY_p;
double kCY_r;
double kCY_da;
double kCY_dr;
double CYo_clean;
double CY_beta_clean;
double CY_p_clean;
double CY_r_clean;
double CY_da_clean;
double CY_dr_clean;
#define kCYo aircraft_->kCYo
#define kCY_beta aircraft_->kCY_beta
#define kCY_p aircraft_->kCY_p
#define kCY_r aircraft_->kCY_r
#define kCY_da aircraft_->kCY_da
#define kCY_dr aircraft_->kCY_dr
#define CYo_clean aircraft_->CYo_clean
#define CY_beta_clean aircraft_->CY_beta_clean
#define CY_p_clean aircraft_->CY_p_clean
#define CY_r_clean aircraft_->CY_r_clean
#define CY_da_clean aircraft_->CY_da_clean
#define CY_dr_clean aircraft_->CY_dr_clean
double kClo;
double kCl_beta;
double kCl_p;
double kCl_r;
double kCl_da;
double kCl_dr;
double Clo_clean;
double Cl_beta_clean;
double Cl_p_clean;
double Cl_r_clean;
double Cl_da_clean;
double Cl_dr_clean;
#define kClo aircraft_->kClo
#define kCl_beta aircraft_->kCl_beta
#define kCl_p aircraft_->kCl_p
#define kCl_r aircraft_->kCl_r
#define kCl_da aircraft_->kCl_da
#define kCl_dr aircraft_->kCl_dr
#define Clo_clean aircraft_->Clo_clean
#define Cl_beta_clean aircraft_->Cl_beta_clean
#define Cl_p_clean aircraft_->Cl_p_clean
#define Cl_r_clean aircraft_->Cl_r_clean
#define Cl_da_clean aircraft_->Cl_da_clean
#define Cl_dr_clean aircraft_->Cl_dr_clean
double kCno;
double kCn_beta;
double kCn_p;
double kCn_r;
double kCn_da;
double kCn_dr;
double Cno_clean;
double Cn_beta_clean;
double Cn_p_clean;
double Cn_r_clean;
double Cn_da_clean;
double Cn_dr_clean;
#define kCno aircraft_->kCno
#define kCn_beta aircraft_->kCn_beta
#define kCn_p aircraft_->kCn_p
#define kCn_r aircraft_->kCn_r
#define kCn_da aircraft_->kCn_da
#define kCn_dr aircraft_->kCn_dr
#define Cno_clean aircraft_->Cno_clean
#define Cn_beta_clean aircraft_->Cn_beta_clean
#define Cn_p_clean aircraft_->Cn_p_clean
#define Cn_r_clean aircraft_->Cn_r_clean
#define Cn_da_clean aircraft_->Cn_da_clean
#define Cn_dr_clean aircraft_->Cn_dr_clean
/* Variables (token2) ===========================================*/
/* record ======== Record desired quantites to file =============*/
map <string,int> record_map;
#define record_map aircraft_->record_map
/***** Forces *******/
double F_X_wind, F_Y_wind, F_Z_wind;
#define F_X_wind aircraft_->F_X_wind
#define F_Y_wind aircraft_->F_Y_wind
#define F_Z_wind aircraft_->F_Z_wind
/* Miscellaneous ================================================*/
int conversion1, conversion2, conversion3;
double confac1, confac2, confac3;
#define conversion1 aircraft_->conversion1
#define conversion2 aircraft_->conversion2
#define conversion3 aircraft_->conversion3
#define confac1 aircraft_->confac1
#define confac2 aircraft_->confac2
#define confac3 aircraft_->confac3
ofstream fout;
#define fout aircraft_->fout
} AIRCRAFT;
// usually defined in the first program that includes uiuc_aircraft.h
extern AIRCRAFT *aircraft_;
#endif // endif _AIRCRAFT_H
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