User talk:Dsekercioglu/MEA
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Principles behind? | 1 | 02:56, 24 September 2017 |
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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)
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