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Aaron


Last seen: 3 years ago Active since 2011

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Problem in converting Mathematica code to Matlab form
Hi greetings all, I'm Aaron and this is the code in Mathematica form : {L, Subscript[M, p], \[Rho], A, Subscript[M, mm]...

13 years ago | 0 answers | 0

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Using Clohessy-Wi;tshire equations to demonstrate the projected circular orbit trajectory base on the initial conditions defined by parameters of Chief Satellite and Deputy Satellite Initial condition
When given a set of parameters for the Chief Satellite with an altitude of 847 km, Eccentricity, e = 0 Orbit inclination, I = ...

14 years ago | 1 answer | 0

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