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A combined Earth scanner and momentum wheel for attitude determination and control of small spacecraftIn order to satisfy the stringent cost and power requirements of small satellites, an advanced SCANWHEEL was designed, built, and qualified by ITHACO, Inc. The T-SCANWHEEL is a modular momentum/reaction wheel with an integral conical Earth scanner. The momentum wheel provides momentum bias and control torques about the pitch axis of a spacecraft. An angled scan mirror coupled to the rotating shaft of the momentum wheel provides a conical scan of the field-of-view of an infrared sensor to provide pitch-and-roll attitude information. By using the same motor and bearings for the momentum wheel and Earth scanner, the overall power consumption is reduced and the system reliability is enhanced. The evolution of the T-SCANWHEEL is presented, including design ground rules, tradeoff analyses, and performance results.
Document ID
19920015835
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bialke, Bill
(Ithaco, Inc. Ithaca, NY, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1992
Publication Information
Publication: NASA. Goddard Space Flight Center, The 26th Aerospace Mechanisms Symposium
Subject Category
Spacecraft Instrumentation
Accession Number
92N25078
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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