Using method developed by C.L.Siegel, G.W.Hill's equations are solved to obtain coordinates of periodic trajectory as Fourier series of time with respect to rotating system of reference; numerical example for satellite of Venus error analysis is undertaken by studying solutions of Hill's equations lying in neighborhood of periodic orbit and corresponding to same value of total energy.
Application of Hill's lunar theory to motion of satellites
J Astronautical Sciences
Journal of the Astronautical Sciences ; 8 , n 2
1961
8 pages
Article (Journal)
English
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