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Time | User | Activity | Comment |
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01:56, 24 September 2017 | Xor (talk | contribs) | Comment text edited | |
01:55, 24 September 2017 | Xor (talk | contribs) | New reply created | (Reply to Principles behind?) |
13:57, 23 September 2017 | Xor (talk | contribs) | New thread created |
in your calculation, you are calculating escape angle theta as theta = v_lateral / (v_bullet - v_retreat)
however, imo this formula is only true when you are moving orbital exactly ;)
Else, you have to calculate some integral, as the change rate of theta is changing everytime the distance changes. (Like my version)