The Collinearity Principle and Minimum Energy Orbits
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: 25 November 2024).
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