The Collinearity Principle and Minimum Energy Orbits

Authors

  • F. P. J. Rimrott
  • W. L. Cleghorn

Abstract

This paper presents two important aspects for application of the Collinearity Principle, viz.: the orbital energy
of a point satellite of constant angular momentum as a function od its orbit eccentricity, and satellite collision.

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Published

2019-10-10

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