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Optimal servicing of geosynchronous satellites

  • Texas A&M University
  • Naval Research Laboratory

Research output: Contribution to conferenceConference paperpeer-review

Abstract

This paper addresses the problem of how to optimally rendezvous with a set of satellites in geosynchronous orbit that have small inclinations. The method developed has application to two problems, servicing of geosynchronous satellites and the removal of dead satellites in geosynchronous orbit. It is shown that when inclination changes are required the optimal solution reduces to the solution of the traveling salesman problem. The method was applied to a set of non-operational geosynchronous satellites selected from the Space Object catalog. The method also directly identifies those satellites that are very costly (in fuel) to visit so that they can be removed from the list to be visited.

Original languageEnglish
Title of host publicationAIAA/AAS Astrodynamics Specialist Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781563479458, 9781624101243
DOIs
StatePublished - 2002
EventAIAA/AAS Astrodynamics Specialist Conference and Exhibit 2002 - Monterey, CA, United States
Duration: 2002.08.52002.08.8

Publication series

NameAIAA/AAS Astrodynamics Specialist Conference and Exhibit

Conference

ConferenceAIAA/AAS Astrodynamics Specialist Conference and Exhibit 2002
Country/TerritoryUnited States
CityMonterey, CA
Period02.08.502.08.8

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