uiuc_2DdataFileReader
02/02/2000 (JS) added record options for 1D and
2D interpolated variables
+ 03/28/2000 (JS) streamlined conversion factors for
+ file readers -- since they are global
+ variables, it is not necessary to put
+ them in the function calls
+ 03/29/2000 (JS) added Cmfa and Weight flags;
+ added misc map; added Dx_cg (etc) to init
+ map
+ 04/01/2000 (JS) added throttle, longitudinal, lateral,
+ and rudder inputs to record map
+ 04/05/2000 (JS) added Altitude to init and record
+ maps; added zero_Long_trim to
+ controlSurface map
+ 03/09/2001 (DPM) added support for gear.
+ 06/18/2001 (RD) Added Alpha, Beta, U_body,
+ V_body, and W_body to init map. Added
+ aileron_input, rudder_input, pilot_elev_no,
+ pilot_ail_no, and pilot_rud_no to
+ controlSurface map. Added Throttle_pct_input
+ to engine map. Added CZfa to CL map.
+ 07/05/2001 (RD) Changed pilot_elev_no = true to pilot_
+ elev_no_check=false. This is to allow pilot
+ to fly aircraft after input files have been
+ used.
+ 08/27/2001 (RD) Added xxx_init_true and xxx_init for
+ P_body, Q_body, R_body, Phi, Theta, Psi,
+ U_body, V_body, and W_body to help in
+ starting the A/C at an initial condition.
+ 10/25/2001 (RD) Added new variables needed for the non-
+ linear Twin Otter model at zero flaps
+ (Cxfxxf0)
+ 11/12/2001 (RD) Added new variables needed for the non-
+ linear Twin Otter model with flaps
+ (Cxfxxf). Removed zero flap variables.
+ Added minmaxfind() which is needed for non-
+ linear variables
+ 01/11/2002 (AP) Added keywords for bootTime
+ 02/13/2002 (RD) Added variables so linear aero model
+ values can be recorded
+ 02/18/2002 (RD) Added variables necessary to use the
+ uiuc_3Dinterp_quick() function. Takes
+ advantage of data in a "nice" form (data
+ that are in a rectangular matrix).
+ 03/13/2002 (RD) Added aircraft_directory so full path
+ is no longer needed in the aircraft.dat file
+ 04/02/2002 (RD) Removed minmaxfind() since it was no
+ longer needed. Added d_2_to_3(),
+ d_1_to_2(), and i_1_to_2() so uiuc_menu()
+ will compile with certain compilers.
+ 08/29/2002 (RD) Separated each primary keyword into its
+ own function to speed up compile time
+ 08/29/2002 (RD w/ help from CO) Made changes to shorten
+ compile time. [] RD to add more comments here.
+ 08/29/2003 (MSS) Adding new keywords for new engine model
+ and slipstream effects on tail.
+ 03/02/2003 (RD) Changed Cxfxxf areas so that there is a
+ conversion factor for flap angle
+ 03/03/2003 (RD) Added flap_cmd_record
+ 03/16/2003 (RD) Added trigger record flags
+ 04/02/2003 (RD) Tokens are now equal to 0 when no value
+ is given in the input file
+ 04/04/2003 (RD) To speed up compile time on this file,
+ each first level token now goes to its
+ own file uiuc_menu_*.cpp
----------------------------------------------------------------------
AUTHOR(S): Bipin Sehgal <bsehgal@uiuc.edu>
- Jeff Scott <jscott@mail.com>
+ Jeff Scott http://www.jeffscott.net/
+ Robert Deters <rdeters@uiuc.edu>
Michael Selig <m-selig@uiuc.edu>
-
+ David Megginson <david@megginson.com>
+ Ann Peedikayil <peedikay@uiuc.edu>
----------------------------------------------------------------------
VARIABLES:
----------------------------------------------------------------------
- CALLED BY: uiuc_wrapper.cpp
+ CALLED BY: uiuc_wrapper.cpp
----------------------------------------------------------------------
CALLS TO: aircraft.dat
tabulated data files (if needed)
+ uiuc_menu_init()
+ uiuc_menu_geometry()
+ uiuc_menu_mass()
+ uiuc_menu_controlSurface()
+ uiuc_menu_CD()
+ uiuc_menu_CL()
+ uiuc_menu_Cm()
+ uiuc_menu_CY()
+ uiuc_menu_Cl()
+ uiuc_menu_Cn()
+ uiuc_menu_ice()
+ uiuc_menu_engine()
+ uiuc_menu_fog()
+ uiuc_menu_gear()
+ uiuc_menu_record()
+ uiuc_menu_misc()
----------------------------------------------------------------------
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.
+ Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA 02110-1301, USA.
**********************************************************************/
+#include <simgear/compiler.h>
+
+
+#include <cstdlib>
+#include <string>
+#include <iostream>
+
#include "uiuc_menu.h"
-bool check_float(string &token)
-{
- float value;
- istrstream stream(token.c_str());
- return (stream >> value);
-}
+using std::cerr;
+using std::cout;
+using std::endl;
+#ifndef _MSC_VER
+using std::exit;
+#endif
-void uiuc_menu (string aircraft_name)
+void uiuc_menu( string aircraft_name )
{
+ string aircraft_directory;
stack command_list;
- double token_value;
- int token_value1, token_value2, token_value3;
-
+
string linetoken1;
string linetoken2;
string linetoken3;
string linetoken4;
string linetoken5;
string linetoken6;
+ string linetoken7;
+ string linetoken8;
+ string linetoken9;
+ string linetoken10;
+ /* the following default setting should eventually be moved to a default or uiuc_init routine */
+
+ recordRate = 1; /* record every time step, default */
+ recordStartTime = 0; /* record from beginning of simulation */
+
+/* set speed at which dynamic pressure terms will be accounted for,
+ since if velocity is too small, coefficients will go to infinity */
+ dyn_on_speed = 33; /* 20 kts (33 ft/sec), default */
+ dyn_on_speed_zero = 0.5 * dyn_on_speed; /* only used if use_dyn_on_speed_curve1 is used */
+ bootindex = 0; // the index for the bootTime
+
/* Read the file and get the list of commands */
airplane = new ParseFile(aircraft_name); /* struct that includes all lines of the input file */
command_list = airplane -> getCommands();
/* structs to include all parts included in the input file for specific keyword groups */
- initParts = new ParseFile();
- geometryParts = new ParseFile();
- massParts = new ParseFile();
- engineParts = new ParseFile();
- aeroParts = new ParseFile();
- gearParts = new ParseFile();
- recordParts = new ParseFile();
+ initParts = new ParseFile();
+ geometryParts = new ParseFile();
+ massParts = new ParseFile();
+ engineParts = new ParseFile();
+ aeroDragParts = new ParseFile();
+ aeroLiftParts = new ParseFile();
+ aeroPitchParts = new ParseFile();
+ aeroSideforceParts = new ParseFile();
+ aeroRollParts = new ParseFile();
+ aeroYawParts = new ParseFile();
+ gearParts = new ParseFile();
+ recordParts = new ParseFile();
if (command_list.begin() == command_list.end())
{
exit(-1);
}
-
+ //construct aircraft-directory
+ aircraft_directory = aircraft_name;
+ int index_aircraft_dat = aircraft_directory.find("aircraft.dat");
+ aircraft_directory.erase(index_aircraft_dat,12);
+
for (LIST command_line = command_list.begin(); command_line!=command_list.end(); ++command_line)
{
cout << *command_line << endl;
-
+
linetoken1 = airplane -> getToken (*command_line, 1);
linetoken2 = airplane -> getToken (*command_line, 2);
+ if (linetoken2=="")
+ linetoken2="0";
linetoken3 = airplane -> getToken (*command_line, 3);
+ if (linetoken3=="")
+ linetoken3="0";
linetoken4 = airplane -> getToken (*command_line, 4);
+ if (linetoken4=="")
+ linetoken4="0";
linetoken5 = airplane -> getToken (*command_line, 5);
+ if (linetoken5=="")
+ linetoken5="0";
linetoken6 = airplane -> getToken (*command_line, 6);
-
- istrstream token3(linetoken3.c_str());
- istrstream token4(linetoken4.c_str());
- istrstream token5(linetoken5.c_str());
- istrstream token6(linetoken6.c_str());
-
- token4 >> token_value1;
- token5 >> token_value2;
- token6 >> token_value3;
+ if (linetoken6=="")
+ linetoken6="0";
+ linetoken7 = airplane -> getToken (*command_line, 7);
+ if (linetoken7=="")
+ linetoken7="0";
+ linetoken8 = airplane -> getToken (*command_line, 8);
+ if (linetoken8=="")
+ linetoken8="0";
+ linetoken9 = airplane -> getToken (*command_line, 9);
+ if (linetoken9=="")
+ linetoken9="0";
+ linetoken10 = airplane -> getToken (*command_line, 10);
+ if (linetoken10=="")
+ linetoken10="0";
+
+ //cout << linetoken1 << endl;
+ //cout << linetoken2 << endl;
+ //cout << linetoken3 << endl;
+ //cout << linetoken4 << endl;
+ //cout << linetoken5 << endl;
+ //cout << linetoken6 << endl;
+ //cout << linetoken7 << endl;
+ //cout << linetoken8 << endl;
+ //cout << linetoken9 << endl;
+ //cout << linetoken10 << endl;
+
+ //istrstream token3(linetoken3.c_str());
+ //istrstream token4(linetoken4.c_str());
+ //istrstream token5(linetoken5.c_str());
+ //istrstream token6(linetoken6.c_str());
+ //istrstream token7(linetoken7.c_str());
+ //istrstream token8(linetoken8.c_str());
+ //istrstream token9(linetoken9.c_str());
+ //istrstream token10(linetoken10.c_str());
switch (Keyword_map[linetoken1])
{
case init_flag:
{
- switch(init_map[linetoken2])
- {
- case Dx_pilot_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Dx_pilot = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case Dy_pilot_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Dy_pilot = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case Dz_pilot_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Dz_pilot = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case V_north_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- V_north = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case V_east_flag:
- {
- initParts -> storeCommands (*command_line);
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- V_east = token_value;
- break;
- }
- case V_down_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- V_down = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case P_body_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- P_body = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case Q_body_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Q_body = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case R_body_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- R_body = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case Phi_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Phi = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case Theta_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Theta = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- case Psi_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Psi = token_value;
- initParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_init( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end init map
-
+
case geometry_flag:
{
- switch(geometry_map[linetoken2])
- {
- case bw_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- bw = token_value;
- geometryParts -> storeCommands (*command_line);
- break;
- }
- case cbar_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- cbar = token_value;
- geometryParts -> storeCommands (*command_line);
- break;
- }
- case Sw_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Sw = token_value;
- geometryParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_geometry( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end geometry map
-
-
+
+
case controlSurface_flag:
{
- switch(controlSurface_map[linetoken2])
- {
- case de_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- demax = token_value;
-
- if (check_float(linetoken4))
- token4 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- demin = token_value;
- break;
- }
- case da_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- damax = token_value;
-
- if (check_float(linetoken4))
- token4 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- damin = token_value;
- break;
- }
- case dr_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- drmax = token_value;
-
- if (check_float(linetoken4))
- token4 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- drmin = token_value;
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_controlSurface( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end controlSurface map
-
-
+
+
case mass_flag:
{
- switch(mass_map[linetoken2])
- {
- case Mass_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Mass = token_value;
- massParts -> storeCommands (*command_line);
- break;
- }
- case I_xx_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- I_xx = token_value;
- massParts -> storeCommands (*command_line);
- break;
- }
- case I_yy_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- I_yy = token_value;
- massParts -> storeCommands (*command_line);
- break;
- }
- case I_zz_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- I_zz = token_value;
- massParts -> storeCommands (*command_line);
- break;
- }
- case I_xz_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- I_xz = token_value;
- massParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_mass( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end mass map
case engine_flag:
{
- switch(engine_map[linetoken2])
- {
- case simpleSingle_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- simpleSingleMaxThrust = token_value;
- engineParts -> storeCommands (*command_line);
- break;
- }
-
- case c172_flag:
- {
- engineParts -> storeCommands (*command_line);
- break;
- }
-
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_engine( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end engine map
case CD_flag:
{
- switch(CD_map[linetoken2])
- {
- case CDo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CDo = token_value;
- CDo_clean = CDo;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CDK_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CDK = token_value;
- CDK_clean = CDK;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CD_a_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CD_a = token_value;
- CD_a_clean = CD_a;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CD_de_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CD_de = token_value;
- CD_de_clean = CD_de;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CDfa_flag:
- {
- CDfa = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- /* call 1D File Reader with file name (CDfa) and conversion
- factors; function returns array of alphas (aArray) and
- corresponding CD values (CDArray) and max number of
- terms in arrays (nAlpha) */
- CDfaData = uiuc_1DdataFileReader(CDfa,
- confac2, /* x */
- confac1, /* y */
- CDfa_aArray,
- CDfa_CDArray,
- CDfa_nAlpha);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CDfade_flag:
- {
- CDfade = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (CDfade) and
- conversion factors; function returns array of
- elevator deflections (deArray) and corresponding
- alpha (aArray) and delta CD (CDArray) values and
- max number of terms in alpha arrays (nAlphaArray)
- and deflection array (nde) */
- CDfadeData = uiuc_2DdataFileReader(CDfade,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- CDfade_aArray,
- CDfade_deArray,
- CDfade_CDArray,
- CDfade_nAlphaArray,
- CDfade_nde);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_CD( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end CD map
+
case CL_flag:
{
- switch(CL_map[linetoken2])
- {
- case CLo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CLo = token_value;
- CLo_clean = CLo;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CL_a_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CL_a = token_value;
- CL_a_clean = CL_a;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CL_adot_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CL_adot = token_value;
- CL_adot_clean = CL_adot;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CL_q_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CL_q = token_value;
- CL_q_clean = CL_q;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CL_de_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CL_de = token_value;
- CL_de_clean = CL_de;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CLfa_flag:
- {
- CLfa = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- /* call 1D File Reader with file name (CLfa) and conversion
- factors; function returns array of alphas (aArray) and
- corresponding CL values (CLArray) and max number of
- terms in arrays (nAlpha) */
- CLfaData = uiuc_1DdataFileReader(CLfa,
- confac2, /* x */
- confac1, /* y */
- CLfa_aArray,
- CLfa_CLArray,
- CLfa_nAlpha);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CLfade_flag:
- {
- CLfade = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (CLfade) and
- conversion factors; function returns array of
- elevator deflections (deArray) and corresponding
- alpha (aArray) and delta CL (CLArray) values and
- max number of terms in alpha arrays (nAlphaArray)
- and deflection array (nde) */
- CLfadeData = uiuc_2DdataFileReader(CLfade,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- CLfade_aArray,
- CLfade_deArray,
- CLfade_CLArray,
- CLfade_nAlphaArray,
- CLfade_nde);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_CL( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end CL map
-
- case Cm_flag:
- {
- switch(Cm_map[linetoken2])
- {
- case Cmo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cmo = token_value;
- Cmo_clean = Cmo;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cm_a_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cm_a = token_value;
- Cm_a_clean = Cm_a;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cm_adot_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
- Cm_adot = token_value;
- Cm_adot_clean = Cm_adot;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cm_q_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
- Cm_q = token_value;
- Cm_q_clean = Cm_q;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cm_de_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cm_de = token_value;
- Cm_de_clean = Cm_de;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cmfade_flag:
- {
- Cmfade = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (Cmfade) and
- conversion factors; function returns array of
- elevator deflections (deArray) and corresponding
- alpha (aArray) and delta Cm (CmArray) values and
- max number of terms in alpha arrays (nAlphaArray)
- and deflection array (nde) */
- CmfadeData = uiuc_2DdataFileReader(Cmfade,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- Cmfade_aArray,
- Cmfade_deArray,
- Cmfade_CmArray,
- Cmfade_nAlphaArray,
- Cmfade_nde);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ case Cm_flag:
+ {
+ parse_Cm( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end Cm map
+
case CY_flag:
{
- switch(CY_map[linetoken2])
- {
- case CYo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CYo = token_value;
- CYo_clean = CYo;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CY_beta_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CY_beta = token_value;
- CY_beta_clean = CY_beta;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CY_p_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CY_p = token_value;
- CY_p_clean = CY_p;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CY_r_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CY_r = token_value;
- CY_r_clean = CY_r;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CY_da_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- CY_da = token_value;
- CY_da_clean = CY_da;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CY_dr_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(2, *command_line);
-
- CY_dr = token_value;
- CY_dr_clean = CY_dr;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CYfada_flag:
- {
- CYfada = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (CYfada) and
- conversion factors; function returns array of
- aileron deflections (daArray) and corresponding
- alpha (aArray) and delta CY (CYArray) values and
- max number of terms in alpha arrays (nAlphaArray)
- and deflection array (nda) */
- CYfadaData = uiuc_2DdataFileReader(CYfada,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- CYfada_aArray,
- CYfada_daArray,
- CYfada_CYArray,
- CYfada_nAlphaArray,
- CYfada_nda);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case CYfbetadr_flag:
- {
- CYfbetadr = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (CYfbetadr) and
- conversion factors; function returns array of
- rudder deflections (drArray) and corresponding
- beta (betaArray) and delta CY (CYArray) values and
- max number of terms in beta arrays (nBetaArray)
- and deflection array (ndr) */
- CYfbetadrData = uiuc_2DdataFileReader(CYfbetadr,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- CYfbetadr_betaArray,
- CYfbetadr_drArray,
- CYfbetadr_CYArray,
- CYfbetadr_nBetaArray,
- CYfbetadr_ndr);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_CY( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end CY map
-
- case Cl_flag:
- {
- switch(Cl_map[linetoken2])
- {
- case Clo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Clo = token_value;
- Clo_clean = Clo;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cl_beta_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
- Cl_beta = token_value;
- Cl_beta_clean = Cl_beta;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cl_p_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
- Cl_p = token_value;
- Cl_p_clean = Cl_p;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cl_r_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cl_r = token_value;
- Cl_r_clean = Cl_r;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cl_da_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cl_da = token_value;
- Cl_da_clean = Cl_da;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cl_dr_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cl_dr = token_value;
- Cl_dr_clean = Cl_dr;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Clfada_flag:
- {
- Clfada = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (Clfada) and
- conversion factors; function returns array of
- aileron deflections (daArray) and corresponding
- alpha (aArray) and delta Cl (ClArray) values and
- max number of terms in alpha arrays (nAlphaArray)
- and deflection array (nda) */
- ClfadaData = uiuc_2DdataFileReader(Clfada,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- Clfada_aArray,
- Clfada_daArray,
- Clfada_ClArray,
- Clfada_nAlphaArray,
- Clfada_nda);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Clfbetadr_flag:
- {
- Clfbetadr = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (Clfbetadr) and
- conversion factors; function returns array of
- rudder deflections (drArray) and corresponding
- beta (betaArray) and delta Cl (ClArray) values and
- max number of terms in beta arrays (nBetaArray)
- and deflection array (ndr) */
- ClfbetadrData = uiuc_2DdataFileReader(Clfbetadr,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- Clfbetadr_betaArray,
- Clfbetadr_drArray,
- Clfbetadr_ClArray,
- Clfbetadr_nBetaArray,
- Clfbetadr_ndr);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ case Cl_flag:
+ {
+ parse_Cl( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end Cl map
- case Cn_flag:
- {
- switch(Cn_map[linetoken2])
- {
- case Cno_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
- Cno = token_value;
- Cno_clean = Cno;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cn_beta_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
- Cn_beta = token_value;
- Cn_beta_clean = Cn_beta;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cn_p_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cn_p = token_value;
- Cn_p_clean = Cn_p;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cn_r_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cn_r = token_value;
- Cn_r_clean = Cn_r;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cn_da_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cn_da = token_value;
- Cn_da_clean = Cn_da;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cn_dr_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- Cn_dr = token_value;
- Cn_dr_clean = Cn_dr;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cnfada_flag:
- {
- Cnfada = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (Cnfada) and
- conversion factors; function returns array of
- aileron deflections (daArray) and corresponding
- alpha (aArray) and delta Cn (CnArray) values and
- max number of terms in alpha arrays (nAlphaArray)
- and deflection array (nda) */
- CnfadaData = uiuc_2DdataFileReader(Cnfada,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- Cnfada_aArray,
- Cnfada_daArray,
- Cnfada_CnArray,
- Cnfada_nAlphaArray,
- Cnfada_nda);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case Cnfbetadr_flag:
- {
- Cnfbetadr = linetoken3;
- conversion1 = token_value1;
- conversion2 = token_value2;
- conversion3 = token_value3;
- confac1 = uiuc_convert(conversion1);
- confac2 = uiuc_convert(conversion2);
- confac3 = uiuc_convert(conversion3);
- /* call 2D File Reader with file name (Cnfbetadr) and
- conversion factors; function returns array of
- rudder deflections (drArray) and corresponding
- beta (betaArray) and delta Cn (CnArray) values and
- max number of terms in beta arrays (nBetaArray)
- and deflection array (ndr) */
- CnfbetadrData = uiuc_2DdataFileReader(Cnfbetadr,
- confac2, /* x */
- confac3, /* y */
- confac1, /* z */
- Cnfbetadr_betaArray,
- Cnfbetadr_drArray,
- Cnfbetadr_CnArray,
- Cnfbetadr_nBetaArray,
- Cnfbetadr_ndr);
- aeroParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ case Cn_flag:
+ {
+ parse_Cn( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end Cn map
- /*
-
case gear_flag:
{
- switch(gear_map[linetoken2])
- {
- case kgear:
- {
- // none yet
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_gear( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
+ break;
} // end gear map
-*/
-
case ice_flag:
{
- switch(ice_map[linetoken2])
- {
- case iceTime_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
-
- else
- uiuc_warnings_errors(1, *command_line);
-
- iceTime = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case transientTime_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- transientTime = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case eta_final_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- eta_final = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case kCDo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCDo = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCDK_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCDK = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCD_a_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCD_a = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCD_de_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCD_de = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case kCLo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCLo = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCL_a_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCL_a = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCL_adot_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCL_adot = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCL_q_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCL_q = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCL_de_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCL_de = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case kCmo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCmo = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCm_a_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCm_a = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCm_adot_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCm_adot = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCm_q_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCm_q = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCm_de_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCm_de = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case kCYo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCYo = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCY_beta_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCY_beta = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCY_p_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCY_p = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCY_r_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCY_r = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCY_da_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCY_da = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCY_dr_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCY_dr = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case kClo_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kClo = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCl_beta_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCl_beta = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCl_p_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCl_p = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCl_r_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCl_r = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCl_da_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCl_da = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCl_dr_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCl_dr = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- case kCno_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCno = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCn_beta_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCn_beta = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCn_p_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCn_p = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCn_r_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCn_r = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCn_da_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCn_da = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
- case kCn_dr_flag:
- {
- if (check_float(linetoken3))
- token3 >> token_value;
- else
- uiuc_warnings_errors(1, *command_line);
-
- kCn_dr = token_value;
- aeroParts -> storeCommands (*command_line);
- break;
- }
-
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_ice( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end ice map
-
+
+
+ case fog_flag:
+ {
+ parse_fog( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
+ break;
+ } // end fog map
+
+
case record_flag:
{
static int fout_flag=0;
fout_flag=-1;
fout.open("uiuc_record.dat");
}
- switch(record_map[linetoken2])
- {
- case Dx_pilot_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
-
- case Dy_pilot_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Dz_pilot_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case V_north_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case V_east_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case V_down_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case V_rel_wind_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Dynamic_pressure_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Alpha_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Alpha_dot_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Beta_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Beta_dot_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Gamma_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case P_body_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Q_body_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case R_body_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Phi_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Theta_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Psi_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Theta_dot_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case density_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Mass_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Simtime_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case dt_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case elevator_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case aileron_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case rudder_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CD_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CDfaI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CDfadeI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CL_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CLfaI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CLfadeI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Cm_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CmfadeI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CY_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CYfadaI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CYfbetadrI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Cl_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case ClfadaI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case ClfbetadrI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case Cn_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CnfadaI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case CnfbetadrI_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_X_wind_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Y_wind_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Z_wind_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_X_aero_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Y_aero_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Z_aero_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_X_engine_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Y_engine_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Z_engine_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_X_gear_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Y_gear_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Z_gear_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_X_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Y_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case F_Z_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_l_aero_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_m_aero_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_n_aero_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_l_engine_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_m_engine_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_n_engine_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_l_gear_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_m_gear_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_n_gear_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_l_rp_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_m_rp_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- case M_n_rp_record:
- {
- recordParts -> storeCommands (*command_line);
- break;
- }
- default:
- {
- uiuc_warnings_errors(2, *command_line);
- break;
- }
- };
+ parse_record( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
break;
} // end record map
-
-
+
+
+ case misc_flag:
+ {
+ parse_misc( linetoken2, linetoken3, linetoken4,
+ linetoken5, linetoken6, linetoken7,
+ linetoken8, linetoken9, linetoken10,
+ aircraft_directory, command_line );
+ break;
+ } // end misc map
+
+
default:
{
if (linetoken1=="*")
return;
- uiuc_warnings_errors(2, *command_line);
+ if (ignore_unknown_keywords) {
+ // do nothing
+ } else {
+ // print error message
+ uiuc_warnings_errors(2, *command_line);
+ }
break;
}
};
projects / flightgear.git / blobdiff