AE4362 Astrodynamics

Review of the two-body problem. The effects of a third point mass and a distributed mass. Expansion of the disturbing potential in series of Legendre functions. Variation of parameter equations for osculating orbital elements. Perturbation and numerical solution techniques. Statistical orbit determination. Codes used by the military to maintain the catalog of artificial satellites and space debris.

Prerequisite

SS3500 or equivalent or by consent of instructor

Lecture Hours

3

Lab Hours

0

Quarter Offered

  • As Required