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Applications of Ergodic Theory to Coverage AnalysisThe study of differential equations, or dynamical systems in general, has two fundamentally different approaches. We are most familiar with the construction of solutions to differential equations. Another approach is to study the statistical behavior of the solutions. Ergodic Theory is one of the most developed methods to study the statistical behavior of the solutions of differential equations. In the theory of satellite orbits, the statistical behavior of the orbits is used to produce 'Coverage Analysis' or how often a spacecraft is in view of a site on the ground. In this paper, we consider the use of Ergodic Theory for Coverage Analysis. This allows us to greatly simplify the computation of quantities such as the total time for which a ground station can see a satellite without ever integrating the trajectory, see Lo 1,2. More over, for any quantity which is an integrable function of the ground track, its average may be computed similarly without the integration of the trajectory. For example, the data rate for a simple telecom system is a function of the distance between the satellite and the ground station. We show that such a function may be averaged using the Ergodic Theorem.
Document ID
20090019038
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Lo, Martin W.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 24, 2013
Publication Date
August 3, 2003
Subject Category
Theoretical Mathematics
Report/Patent Number
AAS03-638
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Big Sky, MT
Country: United States
Start Date: August 3, 2003
End Date: August 7, 2003
Sponsors: American Astronautical Society, American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
Ergodic Theory

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