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Gauge Freedom in Orbital Mechanics MICHAEL EFROIMSKY United States Naval Observatory, Washington DC, USA ABSTRACT: Both orbital and attitude dynamics employ the method of variation of parameters. In a non-perturbed setti
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Document Date: 2014-11-21 14:29:23

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Washington DC / /

Country

United States / /

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U.S. Naval Observatory / Orbital Mechanics MICHAEL EFROIMSKY United States Naval Observatory / /

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gravity law / universal tool / celestial mechanics applications / perturbed gravity law / eventual solution / numerical solution / /

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New York Academy of Sciences / ANNALS NEW YORK ACADEMY OF SCIENCES It / /

Person

Newton / /

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DC / /

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