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Approximations of satellite stabilityModifications and corrections are presented to relations obtained in an investigation conducted by Szebehely (1978), who has discussed the problem of Hill's (1878) stability of satellites in the restricted problem of three bodies. Attention is given to an approximation of the Jacobian constant for the satellite, the critical value of the Jacobian constant, and approximate solutions.
Document ID
19810055518
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Markellos, V. V.
(Glasgow, University Glasgow, United Kingdom)
Szebehely, V.
(Texas, University Austin, TX, United States)
Date Acquired
August 11, 2013
Publication Date
June 1, 1981
Publication Information
Publication: Celestial Mechanics
Volume: 24
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
81A39922
Distribution Limits
Public
Copyright
Other

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