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- W2074112910 abstract "Under the influence of the sun and the moon a highly eccentric orbit of a satellite can become a nearly circular one or a nearly circular orbit might become eccentric. In light of this I suggest a combination of the Gibbsian rotation vector and the Hamiltonian vector as a nonsingular set of elements to be used for all eccentricities and all inclinations. The method of Halphen is suggested for the computation of secular effects, and the method of Liouville for the computation of the near resonance effects caused by the commensurability of mean motions of the disturbed and the disturbing body. The combination of these two methods can give information about the general behavior of the orbit of a minor planet over an interval of some thousands of years, and of an artificial satellite moving in cislunar space over an interval of a number of years." @default.
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- W2074112910 date "1963-12-01" @default.
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- W2074112910 title "On determining the secular and critical effects in the motion of satellites by means of a nonsingular set of vectorial elements" @default.
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- W2074112910 doi "https://doi.org/10.1029/jz068i023p06255" @default.
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