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A Zero-Gyro safemode controller for HSTThe purpose of this paper is to document the Zero-Gyro Sunpoint mode for Hubble Space Telescope, a safemode designed to ensure a power positive state without the use of rate gyros. This paper presents an overview of the Zero-Gyro Sunpoint algorithm, followed by details of the algorithm, control system design, and simulation results. A new, related safemode test, the System Momentum Test, is also discussed.
Document ID
19920072670
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Markley, F. L.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Nelson, John D.
(Lockheed Missiles & Space Co., Inc. Sunnyvale, CA, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 92-4613
Report Number: AIAA PAPER 92-4613
Meeting Information
Meeting: AIAA Guidance, Navigation and Control Conference
Location: Hilton Head Island, SC
Country: United States
Start Date: August 10, 1992
End Date: August 12, 1992
Accession Number
92A55294
Distribution Limits
Public
Copyright
Other

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