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flightgear/src/FDM/UIUCModel/uiuc_menu_CY.cpp

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/**********************************************************************
FILENAME: uiuc_menu_CY.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
06/30/2003 (RD) replaced istrstream with istringstream
to get rid of the annoying warning about
using the strstream header
----------------------------------------------------------------------
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_CY.h"
SG_USING_STD(cerr);
SG_USING_STD(cout);
SG_USING_STD(endl);
#ifndef _MSC_VER
SG_USING_STD(exit);
#endif
void parse_CY( 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;
istringstream token3(linetoken3.c_str());
istringstream token4(linetoken4.c_str());
istringstream token5(linetoken5.c_str());
istringstream token6(linetoken6.c_str());
istringstream token7(linetoken7.c_str());
istringstream token8(linetoken8.c_str());
istringstream token9(linetoken9.c_str());
istringstream token10(linetoken10.c_str());
static bool CYfabetaf_first = true;
static bool CYfadaf_first = true;
static bool CYfadrf_first = true;
static bool CYfapf_first = true;
static bool CYfarf_first = true;
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;
aeroSideforceParts -> 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;
aeroSideforceParts -> 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;
aeroSideforceParts -> 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;
aeroSideforceParts -> 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;
aeroSideforceParts -> 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;
aeroSideforceParts -> storeCommands (*command_line);
break;
}
case CY_dra_flag:
{
if (check_float(linetoken3))
token3 >> token_value;
else
uiuc_warnings_errors(2, *command_line);
CY_dra = token_value;
CY_dra_clean = CY_dra;
aeroSideforceParts -> storeCommands (*command_line);
break;
}
case CY_bdot_flag:
{
if (check_float(linetoken3))
token3 >> token_value;
else
uiuc_warnings_errors(2, *command_line);
CY_bdot = token_value;
CY_bdot_clean = CY_bdot;
aeroSideforceParts -> storeCommands (*command_line);
break;
}
case CYfada_flag:
{
CYfada = 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 (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) */
uiuc_2DdataFileReader(CYfada,
CYfada_aArray,
CYfada_daArray,
CYfada_CYArray,
CYfada_nAlphaArray,
CYfada_nda);
aeroSideforceParts -> storeCommands (*command_line);
break;
}
case CYfbetadr_flag:
{
CYfbetadr = 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 (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) */
uiuc_2DdataFileReader(CYfbetadr,
CYfbetadr_betaArray,
CYfbetadr_drArray,
CYfbetadr_CYArray,
CYfbetadr_nBetaArray,
CYfbetadr_ndr);
aeroSideforceParts -> storeCommands (*command_line);
break;
}
case CYfabetaf_flag:
{
int CYfabetaf_index, i;
string CYfabetaf_file;
double flap_value;
CYfabetaf_file = aircraft_directory + linetoken3;
token4 >> CYfabetaf_index;
if (CYfabetaf_index < 0 || CYfabetaf_index >= 30)
uiuc_warnings_errors(1, *command_line);
if (CYfabetaf_index > CYfabetaf_nf)
CYfabetaf_nf = CYfabetaf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> CYfabetaf_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);
CYfabetaf_fArray[CYfabetaf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (CYfabetaf_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(CYfabetaf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, CYfabetaf_aArray, CYfabetaf_index);
d_1_to_2(datafile_yArray, CYfabetaf_betaArray, CYfabetaf_index);
d_2_to_3(datafile_zArray, CYfabetaf_CYArray, CYfabetaf_index);
i_1_to_2(datafile_nxArray, CYfabetaf_nAlphaArray, CYfabetaf_index);
CYfabetaf_nbeta[CYfabetaf_index] = datafile_ny;
if (CYfabetaf_first==true)
{
if (CYfabetaf_nice == 1)
{
CYfabetaf_na_nice = datafile_nxArray[1];
CYfabetaf_nb_nice = datafile_ny;
d_1_to_1(datafile_yArray, CYfabetaf_bArray_nice);
for (i=1; i<=CYfabetaf_na_nice; i++)
CYfabetaf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroSideforceParts -> storeCommands (*command_line);
CYfabetaf_first=false;
}
break;
}
case CYfadaf_flag:
{
int CYfadaf_index, i;
string CYfadaf_file;
double flap_value;
CYfadaf_file = aircraft_directory + linetoken3;
token4 >> CYfadaf_index;
if (CYfadaf_index < 0 || CYfadaf_index >= 30)
uiuc_warnings_errors(1, *command_line);
if (CYfadaf_index > CYfadaf_nf)
CYfadaf_nf = CYfadaf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> CYfadaf_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);
CYfadaf_fArray[CYfadaf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (CYfadaf_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(CYfadaf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, CYfadaf_aArray, CYfadaf_index);
d_1_to_2(datafile_yArray, CYfadaf_daArray, CYfadaf_index);
d_2_to_3(datafile_zArray, CYfadaf_CYArray, CYfadaf_index);
i_1_to_2(datafile_nxArray, CYfadaf_nAlphaArray, CYfadaf_index);
CYfadaf_nda[CYfadaf_index] = datafile_ny;
if (CYfadaf_first==true)
{
if (CYfadaf_nice == 1)
{
CYfadaf_na_nice = datafile_nxArray[1];
CYfadaf_nda_nice = datafile_ny;
d_1_to_1(datafile_yArray, CYfadaf_daArray_nice);
for (i=1; i<=CYfadaf_na_nice; i++)
CYfadaf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroSideforceParts -> storeCommands (*command_line);
CYfadaf_first=false;
}
break;
}
case CYfadrf_flag:
{
int CYfadrf_index, i;
string CYfadrf_file;
double flap_value;
CYfadrf_file = aircraft_directory + linetoken3;
token4 >> CYfadrf_index;
if (CYfadrf_index < 0 || CYfadrf_index >= 30)
uiuc_warnings_errors(1, *command_line);
if (CYfadrf_index > CYfadrf_nf)
CYfadrf_nf = CYfadrf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> CYfadrf_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);
CYfadrf_fArray[CYfadrf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (CYfadrf_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(CYfadrf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, CYfadrf_aArray, CYfadrf_index);
d_1_to_2(datafile_yArray, CYfadrf_drArray, CYfadrf_index);
d_2_to_3(datafile_zArray, CYfadrf_CYArray, CYfadrf_index);
i_1_to_2(datafile_nxArray, CYfadrf_nAlphaArray, CYfadrf_index);
CYfadrf_ndr[CYfadrf_index] = datafile_ny;
if (CYfadrf_first==true)
{
if (CYfadrf_nice == 1)
{
CYfadrf_na_nice = datafile_nxArray[1];
CYfadrf_ndr_nice = datafile_ny;
d_1_to_1(datafile_yArray, CYfadrf_drArray_nice);
for (i=1; i<=CYfadrf_na_nice; i++)
CYfadrf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroSideforceParts -> storeCommands (*command_line);
CYfadrf_first=false;
}
break;
}
case CYfapf_flag:
{
int CYfapf_index, i;
string CYfapf_file;
double flap_value;
CYfapf_file = aircraft_directory + linetoken3;
token4 >> CYfapf_index;
if (CYfapf_index < 0 || CYfapf_index >= 30)
uiuc_warnings_errors(1, *command_line);
if (CYfapf_index > CYfapf_nf)
CYfapf_nf = CYfapf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> CYfapf_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);
CYfapf_fArray[CYfapf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (CYfapf_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(CYfapf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, CYfapf_aArray, CYfapf_index);
d_1_to_2(datafile_yArray, CYfapf_pArray, CYfapf_index);
d_2_to_3(datafile_zArray, CYfapf_CYArray, CYfapf_index);
i_1_to_2(datafile_nxArray, CYfapf_nAlphaArray, CYfapf_index);
CYfapf_np[CYfapf_index] = datafile_ny;
if (CYfapf_first==true)
{
if (CYfapf_nice == 1)
{
CYfapf_na_nice = datafile_nxArray[1];
CYfapf_np_nice = datafile_ny;
d_1_to_1(datafile_yArray, CYfapf_pArray_nice);
for (i=1; i<=CYfapf_na_nice; i++)
CYfapf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroSideforceParts -> storeCommands (*command_line);
CYfapf_first=false;
}
break;
}
case CYfarf_flag:
{
int CYfarf_index, i;
string CYfarf_file;
double flap_value;
CYfarf_file = aircraft_directory + linetoken3;
token4 >> CYfarf_index;
if (CYfarf_index < 0 || CYfarf_index >= 30)
uiuc_warnings_errors(1, *command_line);
if (CYfarf_index > CYfarf_nf)
CYfarf_nf = CYfarf_index;
token5 >> flap_value;
token6 >> token_value_convert1;
token7 >> token_value_convert2;
token8 >> token_value_convert3;
token9 >> token_value_convert4;
token10 >> CYfarf_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);
CYfarf_fArray[CYfarf_index] = flap_value * convert_f;
/* call 2D File Reader with file name (CYfarf_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(CYfarf_file,
datafile_xArray,
datafile_yArray,
datafile_zArray,
datafile_nxArray,
datafile_ny);
d_2_to_3(datafile_xArray, CYfarf_aArray, CYfarf_index);
d_1_to_2(datafile_yArray, CYfarf_rArray, CYfarf_index);
d_2_to_3(datafile_zArray, CYfarf_CYArray, CYfarf_index);
i_1_to_2(datafile_nxArray, CYfarf_nAlphaArray, CYfarf_index);
CYfarf_nr[CYfarf_index] = datafile_ny;
if (CYfarf_first==true)
{
if (CYfarf_nice == 1)
{
CYfarf_na_nice = datafile_nxArray[1];
CYfarf_nr_nice = datafile_ny;
d_1_to_1(datafile_yArray, CYfarf_rArray_nice);
for (i=1; i<=CYfarf_na_nice; i++)
CYfarf_aArray_nice[i] = datafile_xArray[1][i];
}
aeroSideforceParts -> storeCommands (*command_line);
CYfarf_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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