User contributions
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- 00:36, 6 March 2007 (diff | hist) . . (0) . . Polar file formats (current)
- 00:33, 6 March 2007 (diff | hist) . . (0) . . Category:Aircraft Physics (current)
- 00:24, 6 March 2007 (diff | hist) . . (0) . . Mass.dat
- 00:19, 6 March 2007 (diff | hist) . . (0) . . Category:Aircraft Physics
- 00:17, 6 March 2007 (diff | hist) . . (0) . . Category:Aircraft Physics
- 00:17, 6 March 2007 (diff | hist) . . (0) . . Controls.dat (current)
- 00:16, 6 March 2007 (diff | hist) . . (0) . . N Controls.dat (New page: The purpose of controls.dat is to define the sensitiviy of the controls, and a few other parameters. Here is an example file taken from the Antares model: #----------------------- # Co...)
- 00:12, 6 March 2007 (diff | hist) . . (0) . . N Engine.dat (New page: An optional engine can be defined if the aircraft you are modelling is a motorglider or a towplane. The mathematical engine model is based on a 4-stroke non-turbocharged engine. This is...) (current)
- 00:08, 6 March 2007 (diff | hist) . . (0) . . Category:Aircraft Physics
- 00:06, 6 March 2007 (diff | hist) . . (0) . . Gear.dat
- 00:05, 6 March 2007 (diff | hist) . . (0) . . N Gear.dat (New page: The gear.dat file defines your landing gear, and other points on the aircraft that should collide with the ground. == Gear parts == The file is built up of several gear parts. A typica...)
- 23:46, 5 March 2007 (diff | hist) . . (0) . . Mass.dat
- 23:40, 5 March 2007 (diff | hist) . . (0) . . Polar file formats
- 23:38, 5 March 2007 (diff | hist) . . (0) . . Category:Aircraft Physics
- 23:35, 5 March 2007 (diff | hist) . . (0) . . Mass.dat
- 23:35, 5 March 2007 (diff | hist) . . (0) . . Mass.dat
- 23:34, 5 March 2007 (diff | hist) . . (0) . . Mass.dat
- 23:33, 5 March 2007 (diff | hist) . . (0) . . Mass.dat
- 23:32, 5 March 2007 (diff | hist) . . (0) . . Mass.dat
- 23:13, 5 March 2007 (diff | hist) . . (0) . . N Mass.dat (New page: # Mass system setup mtow = 660 cg_limits = [ 0.290 0.398 ] # Mass of aircraft minus pilot and motor mass { name = fuselage_wings mass = 440.0 inertia =...)
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