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

How to Cite

Rimrott, F. P. J. and Cleghorn, W. L. (2019) “The Collinearity Principle and Minimum Energy Orbits”, Technische Mechanik - European Journal of Engineering Mechanics, 20(4), pp. 305–310. Available at: https://journals.ub.ovgu.de/index.php/techmech/article/view/1103 (Accessed: 18 April 2024).

Issue

Vol. 20 No. 4 (2000)

Section

Article

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