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flightgear/src/FDM/UIUCModel/uiuc_menu_Croll.cpp
curt 7289eaa8ba Robert Deters: 
I have attached some revisions for the UIUCModel and some LaRCsim.
  The only thing you should need to check is LaRCsim.cxx.  The file
  I attached is a revised version of 1.5 and the latest is 1.7.  Also,
  uiuc_getwind.c and uiuc_getwind.h are no longer in the LaRCsim
  directory.  They have been moved over to UIUCModel.
2003-05-13 18:45:04 +00:00

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/**********************************************************************
FILENAME: uiuc_menu_Croll.cpp
----------------------------------------------------------------------
DESCRIPTION: reads input data for specified aircraft and creates
approporiate data storage space
----------------------------------------------------------------------
STATUS: alpha version
----------------------------------------------------------------------
REFERENCES: based on "menu reader" format of Michael Selig
----------------------------------------------------------------------
HISTORY: 04/04/2003 initial release
----------------------------------------------------------------------
AUTHOR(S): Robert Deters <rdeters@uiuc.edu>
Michael Selig <m-selig@uiuc.edu>
----------------------------------------------------------------------
VARIABLES:
----------------------------------------------------------------------
INPUTS: n/a
----------------------------------------------------------------------
OUTPUTS: n/a
----------------------------------------------------------------------
CALLED BY: uiuc_menu()
----------------------------------------------------------------------
CALLS TO: check_float() if needed
d_2_to_3() if needed
d_1_to_2() if needed
i_1_to_2() if needed
d_1_to_1() if needed
----------------------------------------------------------------------
COPYRIGHT: (C) 2003 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.
**********************************************************************/
#include <simgear/compiler.h>
#if defined( __MWERKS__ )
// -dw- optimizer chokes (big-time) trying to optimize humongous
// loop/switch statements
#pragma optimization_level 0
#endif
#include <cstdlib>
#include <string>
#include STL_IOSTREAM
#include "uiuc_menu_Croll.h"
SG_USING_STD(cerr);
SG_USING_STD(cout);
SG_USING_STD(endl);
#ifndef _MSC_VER
SG_USING_STD(exit);
#endif
void parse_Cl( const string& linetoken2, const string& linetoken3,
const string& linetoken4, const string& linetoken5,
const string& linetoken6, const string& linetoken7,
const string& linetoken8, const string& linetoken9,
const string& linetoken10, const string& aircraft_directory,
LIST command_line ) {
double token_value;
int token_value_convert1, token_value_convert2, token_value_convert3;
int token_value_convert4;
double datafile_xArray[100][100], datafile_yArray[100];
double datafile_zArray[100][100];
double convert_f;
int datafile_nxArray[100], datafile_ny;
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());
static bool Clfabetaf_first = true;
static bool Clfadaf_first = true;
static bool Clfadrf_first = true;
static bool Clfapf_first = true;
static bool Clfarf_first = true;
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;
aeroRollParts -> 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;
aeroRollParts -> 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;
aeroRollParts -> 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;
aeroRollParts -> 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;
aeroRollParts -> 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;
aeroRollParts -> storeCommands (*command_line);
break;
}
case Cl_daa_flag:
{
if (check_float(linetoken3))
token3 >> token_value;
else
uiuc_warnings_errors(1, *command_line);
Cl_daa = token_value;
Cl_daa_clean = Cl_daa;
aeroRollParts -> storeCommands (*command_line);
break;
}
case Clfada_flag:
{
Clfada = aircraft_directory + linetoken3;
token4 >> token_value_convert1;
token5 >> token_value_convert2;
token6 >> token_value_convert3;
convert_z = uiuc_convert(token_value_convert1);
convert_x = uiuc_convert(token_value_convert2);
convert_y = uiuc_convert(token_value_convert3);
/* 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) */
uiuc_2DdataFileReader(Clfada,
Clfada_aArray,
Clfada_daArray,
Clfada_ClArray,
Clfada_nAlphaArray,
Clfada_nda);
aeroRollParts -> storeCommands (*command_line);
break;
}
case Clfbetadr_flag:
{
Clfbetadr = aircraft_directory + linetoken3;
token4 >> token_value_convert1;
token5 >> token_value_convert2;
token6 >> token_value_convert3;
convert_z = uiuc_convert(token_value_convert1);
convert_x = uiuc_convert(token_value_convert2);
convert_y = uiuc_convert(token_value_convert3);
/* 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) */
uiuc_2DdataFileReader(Clfbetadr,
Clfbetadr_betaArray,
Clfbetadr_drArray,
Clfbetadr_ClArray,
Clfbetadr_nBetaArray,
Clfbetadr_ndr);
aeroRollParts -> storeCommands (*command_line);
break;
}
case Clfabetaf_flag:
{
int Clfabetaf_index, i;
string Clfabetaf_file;
double flap_value;
Clfabetaf_file = aircraft_directory + linetoken3;
token4 >> Clfabetaf_index;
if (Clfabetaf_index < 0 || Clfabetaf_index >= 100)
uiuc_warnings_errors(1, *command_line);
if (Clfabetaf_index > Clfabetaf_nf)
Clfabetaf_nf = Clfabetaf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> Clfabetaf_nice;
convert_z = uiuc_convert(token_value_convert1);
convert_x = uiuc_convert(token_value_convert2);
convert_y = uiuc_convert(token_value_convert3);
convert_f = uiuc_convert(token_value_convert4);
Clfabetaf_fArray[Clfabetaf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (Clfabetaf_file) and
conversion factors; function returns array of
elevator deflections (deArray) and corresponding
alpha (aArray) and delta CZ (CZArray) values and
max number of terms in alpha arrays (nAlphaArray)
and delfection array (nde) */
uiuc_2DdataFileReader(Clfabetaf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, Clfabetaf_aArray, Clfabetaf_index);
d_1_to_2(datafile_yArray, Clfabetaf_betaArray, Clfabetaf_index);
d_2_to_3(datafile_zArray, Clfabetaf_ClArray, Clfabetaf_index);
i_1_to_2(datafile_nxArray, Clfabetaf_nAlphaArray, Clfabetaf_index);
Clfabetaf_nbeta[Clfabetaf_index] = datafile_ny;
if (Clfabetaf_first==true)
{
if (Clfabetaf_nice == 1)
{
Clfabetaf_na_nice = datafile_nxArray[1];
Clfabetaf_nb_nice = datafile_ny;
d_1_to_1(datafile_yArray, Clfabetaf_bArray_nice);
for (i=1; i<=Clfabetaf_na_nice; i++)
Clfabetaf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroRollParts -> storeCommands (*command_line);
Clfabetaf_first=false;
}
break;
}
case Clfadaf_flag:
{
int Clfadaf_index, i;
string Clfadaf_file;
double flap_value;
Clfadaf_file = aircraft_directory + linetoken3;
token4 >> Clfadaf_index;
if (Clfadaf_index < 0 || Clfadaf_index >= 100)
uiuc_warnings_errors(1, *command_line);
if (Clfadaf_index > Clfadaf_nf)
Clfadaf_nf = Clfadaf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> Clfadaf_nice;
convert_z = uiuc_convert(token_value_convert1);
convert_x = uiuc_convert(token_value_convert2);
convert_y = uiuc_convert(token_value_convert3);
convert_f = uiuc_convert(token_value_convert4);
Clfadaf_fArray[Clfadaf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (Clfadaf_file) and
conversion factors; function returns array of
elevator deflections (deArray) and corresponding
alpha (aArray) and delta CZ (CZArray) values and
max number of terms in alpha arrays (nAlphaArray)
and delfection array (nde) */
uiuc_2DdataFileReader(Clfadaf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, Clfadaf_aArray, Clfadaf_index);
d_1_to_2(datafile_yArray, Clfadaf_daArray, Clfadaf_index);
d_2_to_3(datafile_zArray, Clfadaf_ClArray, Clfadaf_index);
i_1_to_2(datafile_nxArray, Clfadaf_nAlphaArray, Clfadaf_index);
Clfadaf_nda[Clfadaf_index] = datafile_ny;
if (Clfadaf_first==true)
{
if (Clfadaf_nice == 1)
{
Clfadaf_na_nice = datafile_nxArray[1];
Clfadaf_nda_nice = datafile_ny;
d_1_to_1(datafile_yArray, Clfadaf_daArray_nice);
for (i=1; i<=Clfadaf_na_nice; i++)
Clfadaf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroRollParts -> storeCommands (*command_line);
Clfadaf_first=false;
}
break;
}
case Clfadrf_flag:
{
int Clfadrf_index, i;
string Clfadrf_file;
double flap_value;
Clfadrf_file = aircraft_directory + linetoken3;
token4 >> Clfadrf_index;
if (Clfadrf_index < 0 || Clfadrf_index >= 100)
uiuc_warnings_errors(1, *command_line);
if (Clfadrf_index > Clfadrf_nf)
Clfadrf_nf = Clfadrf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> Clfadrf_nice;
convert_z = uiuc_convert(token_value_convert1);
convert_x = uiuc_convert(token_value_convert2);
convert_y = uiuc_convert(token_value_convert3);
convert_f = uiuc_convert(token_value_convert4);
Clfadrf_fArray[Clfadrf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (Clfadrf_file) and
conversion factors; function returns array of
elevator deflections (deArray) and corresponding
alpha (aArray) and delta CZ (CZArray) values and
max number of terms in alpha arrays (nAlphaArray)
and delfection array (nde) */
uiuc_2DdataFileReader(Clfadrf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, Clfadrf_aArray, Clfadrf_index);
d_1_to_2(datafile_yArray, Clfadrf_drArray, Clfadrf_index);
d_2_to_3(datafile_zArray, Clfadrf_ClArray, Clfadrf_index);
i_1_to_2(datafile_nxArray, Clfadrf_nAlphaArray, Clfadrf_index);
Clfadrf_ndr[Clfadrf_index] = datafile_ny;
if (Clfadrf_first==true)
{
if (Clfadrf_nice == 1)
{
Clfadrf_na_nice = datafile_nxArray[1];
Clfadrf_ndr_nice = datafile_ny;
d_1_to_1(datafile_yArray, Clfadrf_drArray_nice);
for (i=1; i<=Clfadrf_na_nice; i++)
Clfadrf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroRollParts -> storeCommands (*command_line);
Clfadrf_first=false;
}
break;
}
case Clfapf_flag:
{
int Clfapf_index, i;
string Clfapf_file;
double flap_value;
Clfapf_file = aircraft_directory + linetoken3;
token4 >> Clfapf_index;
if (Clfapf_index < 0 || Clfapf_index >= 100)
uiuc_warnings_errors(1, *command_line);
if (Clfapf_index > Clfapf_nf)
Clfapf_nf = Clfapf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> Clfapf_nice;
convert_z = uiuc_convert(token_value_convert1);
convert_x = uiuc_convert(token_value_convert2);
convert_y = uiuc_convert(token_value_convert3);
convert_f = uiuc_convert(token_value_convert4);
Clfapf_fArray[Clfapf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (Clfapf_file) and
conversion factors; function returns array of
elevator deflections (deArray) and corresponding
alpha (aArray) and delta CZ (CZArray) values and
max number of terms in alpha arrays (nAlphaArray)
and delfection array (nde) */
uiuc_2DdataFileReader(Clfapf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, Clfapf_aArray, Clfapf_index);
d_1_to_2(datafile_yArray, Clfapf_pArray, Clfapf_index);
d_2_to_3(datafile_zArray, Clfapf_ClArray, Clfapf_index);
i_1_to_2(datafile_nxArray, Clfapf_nAlphaArray, Clfapf_index);
Clfapf_np[Clfapf_index] = datafile_ny;
if (Clfapf_first==true)
{
if (Clfapf_nice == 1)
{
Clfapf_na_nice = datafile_nxArray[1];
Clfapf_np_nice = datafile_ny;
d_1_to_1(datafile_yArray, Clfapf_pArray_nice);
for (i=1; i<=Clfapf_na_nice; i++)
Clfapf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroRollParts -> storeCommands (*command_line);
Clfapf_first=false;
}
break;
}
case Clfarf_flag:
{
int Clfarf_index, i;
string Clfarf_file;
double flap_value;
Clfarf_file = aircraft_directory + linetoken3;
token4 >> Clfarf_index;
if (Clfarf_index < 0 || Clfarf_index >= 100)
uiuc_warnings_errors(1, *command_line);
if (Clfarf_index > Clfarf_nf)
Clfarf_nf = Clfarf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> Clfarf_nice;
convert_z = uiuc_convert(token_value_convert1);
convert_x = uiuc_convert(token_value_convert2);
convert_y = uiuc_convert(token_value_convert3);
convert_f = uiuc_convert(token_value_convert4);
Clfarf_fArray[Clfarf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (Clfarf_file) and
conversion factors; function returns array of
elevator deflections (deArray) and corresponding
alpha (aArray) and delta CZ (CZArray) values and
max number of terms in alpha arrays (nAlphaArray)
and delfection array (nde) */
uiuc_2DdataFileReader(Clfarf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, Clfarf_aArray, Clfarf_index);
d_1_to_2(datafile_yArray, Clfarf_rArray, Clfarf_index);
d_2_to_3(datafile_zArray, Clfarf_ClArray, Clfarf_index);
i_1_to_2(datafile_nxArray, Clfarf_nAlphaArray, Clfarf_index);
Clfarf_nr[Clfarf_index] = datafile_ny;
if (Clfarf_first==true)
{
if (Clfarf_nice == 1)
{
Clfarf_na_nice = datafile_nxArray[1];
Clfarf_nr_nice = datafile_ny;
d_1_to_1(datafile_yArray, Clfarf_rArray_nice);
for (i=1; i<=Clfarf_na_nice; i++)
Clfarf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroRollParts -> storeCommands (*command_line);
Clfarf_first=false;
}
break;
}
default:
{
if (ignore_unknown_keywords) {
// do nothing
} else {
// print error message
uiuc_warnings_errors(2, *command_line);
}
break;
}
};
}
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