Run TARC payloader simulation and save new simulation data. I compared our simulation data with an on-line descent rate calculator at https://descentratecalculator.onlinetesting.net/ and saw that the results are well within 1 fps of each other.
Updated Tube Fin example to include basic required components to function correctly... streamer decent rate too high (substituted parachute), no engine block or launch lug. Changes also re-ran simulation and eliminated tube fin warning.
changed nose cone and transition shoulder diameters to be consistent with body tube inner diameter; changed parachute characteristics to reduce decent to appropriate rate; moved centering forward and middle centering rings to ends of fins; changed fin tabs to be consistent with 15.03; rotated launch lugs so that rod is not going through fins.
- Simulations now load the configuration ids corresponding to it's file entry.
- involved removing redundand flightconfig id fields
- FROM simulation conditions and simulation options
- TO "Simulation"
- Distilled some unit tests to use all rockets from the TestRocket class.
- Fixed a few warnings
Separate swing application code from core code. Moved a bunch of sources
and libraries around. Created new eclipse project.
Further refinements to make it build.
Update gitignore.
