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Development of control systems for space shuttle vehicles, volume 1Control of winged two-stage space shuttle vehicles was investigated. Control requirements were determined and systems capable of meeting these requirements were synthesized. Control requirements unique to shuttles were identified. It is shown that these requirements can be satisfied by conventional control logics. Linear gain schedule controllers predominate. Actuator saturations require nonlinear compensation in some of the control systems.
Document ID
19720003296
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stone, C. R. (Honeywell, Inc. Minneapolis, MN, United States)
Chase, T. W. (Honeywell, Inc. Minneapolis, MN, United States)
Kiziloz, B. M. (Honeywell, Inc. Minneapolis, MN, United States)
Skelley, E. D. (Honeywell, Inc. Minneapolis, MN, United States)
Stein, G. (Honeywell, Inc. Minneapolis, MN, United States)
Ward, M. D. (Honeywell, Inc. Minneapolis, MN, United States)
Skelton, G. B. (Honeywell, Inc. Minneapolis, MN, United States)
Yore, E. E. (Honeywell, Inc. Minneapolis, MN, United States)
Rupert, J. G. (Honeywell, Inc. Minneapolis, MN, United States)
Phelps, R. K. (Honeywell, Inc. Minneapolis, MN, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1971
Publication Information
Publisher: NASA
Subject Category
Space Vehicles
Report/Patent Number
HONEYWELL-14257-FR-VOL-1
NASA-CR-1899
Accession Number
72N10945
Funding Number(s)
CONTRACT_GRANT: NAS8-25181
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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