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.

Downloads

Published

2019-10-10

Issue

Vol. 20 No. 4 (2000)

Section

Article

Most read articles by the same author(s)

1 2 3 > >>