Accession Number:

ADA496753

Title:

Application of KAM Theorem to Earth Orbiting Satellites

Descriptive Note:

Master's thesis

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH DEPT OF AERONAUTICS AND ASTRONAUTICS

Personal Author(s):

Report Date:

2009-03-01

Pagination or Media Count:

61.0

Abstract:

An orbit that lies on a Kolmogorov, Arnold, and Moser KAM Torus will remain on that torus until and unless it experiences a force that causes it to leave the torus. Earth satellites that are subject only to the Earths gravity field may lie on such KAM tori. Analyzing on orbit satellite position data should allow for the identification of the fundamental frequencies needed to define the KAM tori for modeling Earth satellite orbits. KAM Tori are created for the Gravity Recovery and Climate Experience GRACE and Jason-1 satellites to model their orbital motion. Precise position data for the satellites is analyzed using a modified Laskar frequency algorithm to determine the fundamental frequencies of the orbits. The fundamental frequencies along with a set of Fourier coefficients completely describe the tori. These tori are then compared to the precise orbital position data for the satellites to determine how well they model the orbits. The KAM torus created for the Jason-1 satellite is able to represent the position of the satellites to within 1 km. Further refinement of the torus should be possible, resulting in a more accurate model of the orbit. The GRACE torus was less successful at determining the satellite positions. Atmospheric drag cannot be ignored at the altitude where GRACE flies. It may still be possible to model GRACE with a KAM torus by applying perturbation theory to the torus however, further research is needed to confirm this.

Subject Categories:

  • Spacecraft Trajectories and Reentry

Distribution Statement:

APPROVED FOR PUBLIC RELEASE