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Dual keel Space Station payload pointing system design and analysis feasibility studyA Space Station attached Payload Pointing System (PPS) has been designed and analyzed. The PPS is responsible for maintaining fixed payload pointing in the presence of disturbance applied to the Space Station. The payload considered in this analysis is the Solar Optical Telescope. System performance is evaluated via digital time simulations by applying various disturbance forces to the Space Station. The PPS meets the Space Station articulated pointing requirement for all disturbances except Shuttle docking and some centrifuge cases.
Document ID
19890028477
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Smagala, Tom
(Fairchild Space and Electronics Co. Germantown, MD, United States)
Class, Brian F.
(Fairchild Space Co. Germantown MD, United States)
Bauer, Frank H.
(Fairchild Space and Electronics Co. Germantown, MD, United States)
Lebair, Deborah A.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1988
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Acquisition, Tracking, and Pointing II
Location: Los Angeles, CA
Country: United States
Start Date: January 14, 1988
End Date: January 15, 1988
Sponsors: SPIE
Accession Number
89A15848
Distribution Limits
Public
Copyright
Other

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