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
|
