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@ -5,29 +5,22 @@ Manual TODO file, no claude's allowed!
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=== Project Documentation === |
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- remember to periodically check the reference docs against new changes |
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=== Simulation/Physics === |
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- remove bodies on non closed orbits after they are a certain distance from |
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the root body, or bary-center |
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- add tests for each orbit type |
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=== CTAGS === |
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- previously we've used the Makefile to generate tags when building, |
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let's think about a way we can generate them without causing a conflict |
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for people who don't use ctags |
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=== Simulation Config Files === |
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- decide on an easier to read format, likely TOML or JSON |
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- the config_loader module needs to be refactored, and likely needs some |
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logic moved to the bodies module (which should probably be renamed |
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simulation) |
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=== Orbital Mechanics/Physics === |
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- change orbit propagation method to Newton-Raphson |
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- tell claude to move any updated changes into 'staging' block comment for |
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easier review, and for later refactoring |
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- find some test data for solar system object orbits for verification |
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- also need tests for circular orbits, and orbits which might have anomalies |
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with simple trig equations |
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- test for orbit state after many revolutions |
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- a nice concise reference doc: https://web.mit.edu/10.001/Web/Course_Notes/NLAE/node6.html |
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- lastly test with different time steps to find an 'acceptable' error that's |
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pretty accurate, but doesn't take too many iterations. I used < 10 |
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originally in orbital_shipping |
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- parabolic, and hyperbolic orbits with tests |
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=== rendereing === |
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- for starters, the minimum scaling of objects should be replaced with some |
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kind of billboard system |
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