/********************************************************************** FILENAME: uiuc_menu_Cm.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_Cm.h" SG_USING_STD(cerr); SG_USING_STD(cout); SG_USING_STD(endl); #ifndef _MSC_VER SG_USING_STD(exit); #endif void parse_Cm( 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 Cmfabetaf_first = true; static bool Cmfadef_first = true; static bool Cmfaqf_first = true; 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; aeroPitchParts -> 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; aeroPitchParts -> storeCommands (*command_line); break; } case Cm_a2_flag: { if (check_float(linetoken3)) token3 >> token_value; else uiuc_warnings_errors(1, *command_line); Cm_a2 = token_value; Cm_a2_clean = Cm_a2; aeroPitchParts -> 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; aeroPitchParts -> 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; aeroPitchParts -> storeCommands (*command_line); break; } case Cm_ih_flag: { if (check_float(linetoken3)) token3 >> token_value; else uiuc_warnings_errors(1, *command_line); Cm_ih = token_value; aeroPitchParts -> 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; aeroPitchParts -> storeCommands (*command_line); break; } case Cm_b2_flag: { if (check_float(linetoken3)) token3 >> token_value; else uiuc_warnings_errors(1, *command_line); Cm_b2 = token_value; Cm_b2_clean = Cm_b2; aeroPitchParts -> storeCommands (*command_line); break; } case Cm_r_flag: { if (check_float(linetoken3)) token3 >> token_value; else uiuc_warnings_errors(1, *command_line); Cm_r = token_value; Cm_r_clean = Cm_r; aeroPitchParts -> storeCommands (*command_line); break; } case Cm_df_flag: { if (check_float(linetoken3)) token3 >> token_value; else uiuc_warnings_errors(1, *command_line); Cm_df = token_value; Cm_df_clean = Cm_df; aeroPitchParts -> storeCommands (*command_line); break; } case Cm_ds_flag: { if (check_float(linetoken3)) token3 >> token_value; else uiuc_warnings_errors(1, *command_line); Cm_ds = token_value; aeroPitchParts -> storeCommands (*command_line); break; } case Cm_dg_flag: { if (check_float(linetoken3)) token3 >> token_value; else uiuc_warnings_errors(1, *command_line); Cm_dg = token_value; aeroPitchParts -> storeCommands (*command_line); break; } case Cmfa_flag: { Cmfa = aircraft_directory + linetoken3; token4 >> token_value_convert1; token5 >> token_value_convert2; convert_y = uiuc_convert(token_value_convert1); convert_x = uiuc_convert(token_value_convert2); /* call 1D File Reader with file name (Cmfa) and conversion factors; function returns array of alphas (aArray) and corresponding Cm values (CmArray) and max number of terms in arrays (nAlpha) */ uiuc_1DdataFileReader(Cmfa, Cmfa_aArray, Cmfa_CmArray, Cmfa_nAlpha); aeroPitchParts -> storeCommands (*command_line); break; } case Cmfade_flag: { Cmfade = 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 (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) */ uiuc_2DdataFileReader(Cmfade, Cmfade_aArray, Cmfade_deArray, Cmfade_CmArray, Cmfade_nAlphaArray, Cmfade_nde); aeroPitchParts -> storeCommands (*command_line); break; } case Cmfdf_flag: { Cmfdf = aircraft_directory + linetoken3; token4 >> token_value_convert1; token5 >> token_value_convert2; convert_y = uiuc_convert(token_value_convert1); convert_x = uiuc_convert(token_value_convert2); /* call 1D File Reader with file name (Cmfdf) and conversion factors; function returns array of dfs (dfArray) and corresponding Cm values (CmArray) and max number of terms in arrays (ndf) */ uiuc_1DdataFileReader(Cmfdf, Cmfdf_dfArray, Cmfdf_CmArray, Cmfdf_ndf); aeroPitchParts -> storeCommands (*command_line); break; } case Cmfadf_flag: { Cmfadf = 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 (Cmfadf) and conversion factors; function returns array of flap deflections (dfArray) and corresponding alpha (aArray) and delta Cm (CmArray) values and max number of terms in alpha arrays (nAlphaArray) and deflection array (ndf) */ uiuc_2DdataFileReader(Cmfadf, Cmfadf_aArray, Cmfadf_dfArray, Cmfadf_CmArray, Cmfadf_nAlphaArray, Cmfadf_ndf); aeroPitchParts -> storeCommands (*command_line); break; } case Cmfabetaf_flag: { int Cmfabetaf_index, i; string Cmfabetaf_file; double flap_value; Cmfabetaf_file = aircraft_directory + linetoken3; token4 >> Cmfabetaf_index; if (Cmfabetaf_index < 0 || Cmfabetaf_index >= 30) uiuc_warnings_errors(1, *command_line); if (Cmfabetaf_index > Cmfabetaf_nf) Cmfabetaf_nf = Cmfabetaf_index; token5 >> flap_value; token6 >> token_value_convert1; token7 >> token_value_convert2; token8 >> token_value_convert3; token9 >> token_value_convert4; token10 >> Cmfabetaf_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); Cmfabetaf_fArray[Cmfabetaf_index] = flap_value * convert_f; /* call 2D File Reader with file name (Cmfabetaf_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(Cmfabetaf_file, datafile_xArray, datafile_yArray, datafile_zArray, datafile_nxArray, datafile_ny); d_2_to_3(datafile_xArray, Cmfabetaf_aArray, Cmfabetaf_index); d_1_to_2(datafile_yArray, Cmfabetaf_betaArray, Cmfabetaf_index); d_2_to_3(datafile_zArray, Cmfabetaf_CmArray, Cmfabetaf_index); i_1_to_2(datafile_nxArray, Cmfabetaf_nAlphaArray, Cmfabetaf_index); Cmfabetaf_nbeta[Cmfabetaf_index] = datafile_ny; if (Cmfabetaf_first==true) { if (Cmfabetaf_nice == 1) { Cmfabetaf_na_nice = datafile_nxArray[1]; Cmfabetaf_nb_nice = datafile_ny; d_1_to_1(datafile_yArray, Cmfabetaf_bArray_nice); for (i=1; i<=Cmfabetaf_na_nice; i++) Cmfabetaf_aArray_nice[i] = datafile_xArray[1][i]; } aeroPitchParts -> storeCommands (*command_line); Cmfabetaf_first=false; } break; } case Cmfadef_flag: { int Cmfadef_index, i; string Cmfadef_file; double flap_value; Cmfadef_file = aircraft_directory + linetoken3; token4 >> Cmfadef_index; if (Cmfadef_index < 0 || Cmfadef_index >= 30) uiuc_warnings_errors(1, *command_line); if (Cmfadef_index > Cmfadef_nf) Cmfadef_nf = Cmfadef_index; token5 >> flap_value; token6 >> token_value_convert1; token7 >> token_value_convert2; token8 >> token_value_convert3; token9 >> token_value_convert4; token10 >> Cmfadef_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); Cmfadef_fArray[Cmfadef_index] = flap_value * convert_f; /* call 2D File Reader with file name (Cmfadef_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(Cmfadef_file, datafile_xArray, datafile_yArray, datafile_zArray, datafile_nxArray, datafile_ny); d_2_to_3(datafile_xArray, Cmfadef_aArray, Cmfadef_index); d_1_to_2(datafile_yArray, Cmfadef_deArray, Cmfadef_index); d_2_to_3(datafile_zArray, Cmfadef_CmArray, Cmfadef_index); i_1_to_2(datafile_nxArray, Cmfadef_nAlphaArray, Cmfadef_index); Cmfadef_nde[Cmfadef_index] = datafile_ny; if (Cmfadef_first==true) { if (Cmfadef_nice == 1) { Cmfadef_na_nice = datafile_nxArray[1]; Cmfadef_nde_nice = datafile_ny; d_1_to_1(datafile_yArray, Cmfadef_deArray_nice); for (i=1; i<=Cmfadef_na_nice; i++) Cmfadef_aArray_nice[i] = datafile_xArray[1][i]; } aeroPitchParts -> storeCommands (*command_line); Cmfadef_first=false; } break; } case Cmfaqf_flag: { int Cmfaqf_index, i; string Cmfaqf_file; double flap_value; Cmfaqf_file = aircraft_directory + linetoken3; token4 >> Cmfaqf_index; if (Cmfaqf_index < 0 || Cmfaqf_index >= 30) uiuc_warnings_errors(1, *command_line); if (Cmfaqf_index > Cmfaqf_nf) Cmfaqf_nf = Cmfaqf_index; token5 >> flap_value; token6 >> token_value_convert1; token7 >> token_value_convert2; token8 >> token_value_convert3; token9 >> token_value_convert4; token10 >> Cmfaqf_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); Cmfaqf_fArray[Cmfaqf_index] = flap_value * convert_f; /* call 2D File Reader with file name (Cmfaqf_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(Cmfaqf_file, datafile_xArray, datafile_yArray, datafile_zArray, datafile_nxArray, datafile_ny); d_2_to_3(datafile_xArray, Cmfaqf_aArray, Cmfaqf_index); d_1_to_2(datafile_yArray, Cmfaqf_qArray, Cmfaqf_index); d_2_to_3(datafile_zArray, Cmfaqf_CmArray, Cmfaqf_index); i_1_to_2(datafile_nxArray, Cmfaqf_nAlphaArray, Cmfaqf_index); Cmfaqf_nq[Cmfaqf_index] = datafile_ny; if (Cmfaqf_first==true) { if (Cmfaqf_nice == 1) { Cmfaqf_na_nice = datafile_nxArray[1]; Cmfaqf_nq_nice = datafile_ny; d_1_to_1(datafile_yArray, Cmfaqf_qArray_nice); for (i=1; i<=Cmfaqf_na_nice; i++) Cmfaqf_aArray_nice[i] = datafile_xArray[1][i]; } aeroPitchParts -> storeCommands (*command_line); Cmfaqf_first=false; } break; } default: { if (ignore_unknown_keywords) { // do nothing } else { // print error message uiuc_warnings_errors(2, *command_line); } break; } }; }