Physics
Scientist
Joint Publications Research Service, Arlington, VA.
A condition for the boundedness of a spacecraft's orbit in the vicinity of a collinear libration center of the restricted elliptical three-body problem
Control of motion of a space vehicle in the neighbourhood of the collinear libration centre in the restricted elliptical three-body problem.
Limitation of spacecraft orbit near colinear libration center of limited elliptical three body problem
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