Course #AE4362

Est.imated Completion Time: 3 months


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.

Included in degrees & certificates

  • 299


  • SS3500
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Academic Calendar

  •  09 Jun 2023

    Spring quarter last day of classes

  •  13 Jun 2023

    Spring quarter final examinations begin

  •  15 Jun 2023

    Spring quarter final examinations end