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Applying EVM to Satellite on Ground and In-Orbit Testing - Better Data in Less TimeUsing Error Vector Magnitude (EVM) in satellite integration and test allows rapid verification of the Bit Error Rate (BER) performance of a satellite link and is particularly well suited to measurement of low bit rate satellite links where it can result in a major reduction in test time (about 3 weeks per satellite for the Geosynchronous Operational Environmental Satellite [GOES] satellites during ground test) and can provide diagnostic information. Empirical techniques developed to predict BER performance from EVM measurements and lessons learned about applying these techniques during GOES N, O, and P integration test and post launch testing, are discussed.
Document ID
20080023284
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Peters, Robert
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Lebbink, Elizabeth-Klein
(Boeing Integrated Defense Systems El Segundo, CA, United States)
Lee, Victor
(Boeing Integrated Defense Systems El Segundo, CA, United States)
Model, Josh
(Lincoln Labs. Lexington, MA, United States)
Wezalis, Robert
(Lincoln Labs. Lexington, MA, United States)
Taylor, John
(Lincoln Labs. Lexington, MA, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Communications And Radar
Distribution Limits
Public
Copyright
Public Use Permitted.
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