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    A note on a Lagrangian formulation for motion about the collinear points (1980)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: A Lagrangian formulation for the three-dimensional motion of a satellite in the vicinity of the collinear points of the circular-restricted problem is reconsidered. It is shown that the influence of the primaries can be expressed in the form of two third-body disturbing functions. By use of this approach, the equations for the Lagrangian and for the motion itself are readily developed into highly compact expressions. All orders of the non-linear developments are shown to be easily obtainable using well-known recursive relationships. The resulting forms for these equations are well suited for use in the initial phase of canonical or non-canonical investigations.
    Keywords: ASTRODYNAMICS
    Type: Celestial Mechanics; 22; Oct. 198
    Format: text
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