/********************************************************************** 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 ---------------------------------------------------------------------- AUTHOR(S): Robert Deters Michael Selig ---------------------------------------------------------------------- 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 #if defined( __MWERKS__ ) // -dw- optimizer chokes (big-time) trying to optimize humongous // loop/switch statements #pragma optimization_level 0 #endif #include #include #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; 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 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; } }; }