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From: <mk...@us...> - 2003-04-11 23:43:08
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Update of /cvsroot/csp/APPLICATIONS/CSPSim In directory sc8-pr-cvs1:/tmp/cvs-serv5133 Modified Files: CHANGES.current Log Message: see CHANGES.current Index: CHANGES.current =================================================================== RCS file: /cvsroot/csp/APPLICATIONS/CSPSim/CHANGES.current,v retrieving revision 1.15 retrieving revision 1.16 diff -C2 -d -r1.15 -r1.16 *** CHANGES.current 11 Apr 2003 19:33:03 -0000 1.15 --- CHANGES.current 11 Apr 2003 23:43:05 -0000 1.16 *************** *** 2,8 **** =========================== ! ALL USERS: you will need to remake your aircraft.hid file. ! Go to Tools/HID, and run map2hid aicraft.map, then copy the ! resulting aicraft.hid file to your Data/Input directory. 2003-04-10: onsight --- 2,30 ---- =========================== ! 2003-04-11: onsight ! Fixed two coordinate system bugs in the impact code during ! hard crashes that could cause numerical overflows and lead ! to segfaults. There's still somewhat odd behaviour at ! times, but only under conditions where the plane would ! break into pieces anyway (which of course isn't modelled ! yet). ! ! Reordered member initializers in NumericalMethod ctors to ! silence gcc warnigns. ! ! Made DynamicalSystem dtor virtual. ! ! Added global try/catch block around CSPSim::Init. ! ! Added trilinear filtering option to ObjectModel. ! ! Added #! shell escape to the python scripts in Bin ! so they can be run directly from the commandd line ! under linux (assuming your python path is the same ! as mine ;-). ! ! *********** ALL USERS: you will need to remake your aircraft.hid file. ! Go to Tools/HID, and run map2hid aicraft.map, then copy the ! resulting aicraft.hid file to your Data/Input directory. 2003-04-10: onsight *************** *** 17,21 **** when binding to the m2k and other aircraft. ! LINUX USERS: you need to add NumericalMethod.cpp to your Makefile. 2003-04-09: delta updated .net project. --- 39,45 ---- when binding to the m2k and other aircraft. ! *********** LINUX USERS: you need to add NumericalMethod.cpp to your ! Makefile. ! 2003-04-09: delta updated .net project. *************** *** 24,46 **** updated .net project; debug and release are maintained. ! Rewritten DynamicalSystem interface; you need now, to define a ! vector field as a method of DynamicalSystem (which inherites from ! VectorField). You need to furnish the NumericalMethod used to approximate ! the exact solution of your ODE (use setNumericalMethod). AeroDynamics is ! now a DynamicalSystem. ! Merging Onsight code on airflow, collision and landing gear; this code is not ! yet enabled. ! Cleaning code in CSPSim.cpp, AeroDynamics.cpp and .h; added NumericalMethod.cpp ! and NumericalMethod.h. 2003-03-28: delta ! .net project updated: CSPSimDLL (release mode is maintained) ! You can run python scripts from commandline without invoking python ! interpreter. For example, to rebuild data: "RebuildData.py <CR>" or ! to run CSP, "CSPSim.py <CR>". ! Removed CSPWin.py, CompileData.py and RebuildData.py from /VisualStudio. 2003-03-27: onsight --- 48,71 ---- updated .net project; debug and release are maintained. ! Rewritten DynamicalSystem interface; you need now, to define a ! vector field as a method of DynamicalSystem (which inherites ! from VectorField). You need to furnish the NumericalMethod used ! to approximate the exact solution of your ODE (use ! setNumericalMethod). AeroDynamics is now a DynamicalSystem. ! Merging Onsight code on airflow, collision and landing gear; ! this code is not yet enabled. ! Cleaning code in CSPSim.cpp, AeroDynamics.cpp and .h; added ! NumericalMethod.cpp and NumericalMethod.h. 2003-03-28: delta ! .net project updated: CSPSimDLL (release mode is maintained) You ! can run python scripts from commandline without invoking python ! interpreter. For example, to rebuild data: "RebuildData.py <CR>" ! or to run CSP, "CSPSim.py <CR>". ! Removed CSPWin.py, CompileData.py and RebuildData.py from ! /VisualStudio. 2003-03-27: onsight |