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Orbit design and optimization based on global telecommunication performance metricsThe orbit selection of telecommunications orbiters is one of the critical design processes and should be guided by global telecom performance metrics and mission-specific constraints. In order to aid the orbit selection, we have coupled the Telecom Orbit Analysis and Simulation Tool (TOAST) with genetic optimization algorithms. As a demonstration, we have applied the developed tool to select an optimal orbit for general Mars telecommunications orbiters with the constraint of being a frozen orbit. While a typical optimization goal is to minimize tele-communications down time, several relevant performance metrics are examined: 1) area-weighted average gap time, 2) global maximum of local maximum gap time, 3) global maximum of local minimum gap time. Optimal solutions are found with each of the metrics. Common and different features among the optimal solutions as well as the advantage and disadvantage of each metric are presented. The optimal solutions are compared with several candidate orbits that were considered during the development of Mars Telecommunications Orbiter.
Document ID
20060043984
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Lee, Seungwon
Lee, Charles H.
Kerridge, Stuart
Cheung, Kar-Ming
Edwards, Charles D.
Date Acquired
August 23, 2013
Publication Date
March 4, 2006
Subject Category
Communications And Radar
Meeting Information
Meeting: IEEE Aerospace Conference
Location: Big Sky, MT
Country: United States
Start Date: March 4, 2006
End Date: March 11, 2006
Distribution Limits
Public
Copyright
Other
Keywords
genetic algorithms
telecommunications orbiters

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