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Satellite GN and C Anomaly TrendsOn-orbit anomaly records for satellites launched from 1990 through 2001 are reviewed to determine recent trends of un-manned space mission critical failures. Anomalies categorized by subsystems show that Guidance, Navigation and Control (GN&C) subsystems have a high number of anomalies that result in a mission critical failure when compared to other subsystems. A mission critical failure is defined as a premature loss of a satellite or loss of its ability to perform its primary mission during its design life. The majority of anomalies are shown to occur early in the mission, usually within one year from launch. GN&C anomalies are categorized by cause and equipment type involved. A statistical analysis of the data is presented for all anomalies compared with the GN&C anomalies for various mission types, orbits and time periods. Conclusions and recommendations are presented for improving mission success and reliability.
Document ID
20030025663
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Robertson, Brent
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Stoneking, Eric
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2003
Subject Category
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
AAS-03-071
Meeting Information
Meeting: 2003 AAS Guidance and Control Conference
Location: Breckenridge, CO
Country: United States
Start Date: February 5, 2003
End Date: February 9, 2003
Sponsors: American Astronomical Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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