On the 75th birthday of A.P.Markeev
Hillís curves and libration points in the low-thrust restricted circular threebody problem
P. S. Krasil'nikov
Moscow Aviation Institute (National Research University), Volokolamskoe sh. 4, GSP-3, A-80, Moscow, 125993, Russia
The plane circular restricted three-body problem is considered, where the massless body is a constant low-thrust spacecraft. It is assumed that the vector of low-thrust is directed along the $Ox$ axis connecting the main bodies. The problem of plotting a family of one-parameter Hillís curves is investigated. The existence conditions of artificial triangular-type and collineartype libration points are obtained. The values of the effective force function at libration points are investigated also. Six different topological types of the family of one-parameter Hillís curves are described. It is shown that these types differ in the number of critical values of the constant Jacobi integral and in the ordering of these values. For the Earth Ė Moon system, a family of one-parameter Hillís curves is plotted for each of the six types.
restricted three-body problem, Hillís curves, libration points, constant low-thrust spacecraft
PDF file (2586 kB)
MSC: 70F07, 70K42, 53A04
P. S. Krasil'nikov, “Hillís curves and libration points in the low-thrust restricted circular threebody problem”, Nelin. Dinam., 13:4 (2017), 543–556
Citation in format AMSBIB
\paper Hillís curves and libration points in the low-thrust restricted circular threebody problem
\jour Nelin. Dinam.
Citing articles on Google Scholar:
Related articles on Google Scholar:
|Number of views:|