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Space shuttle digital flight control systemThe space shuttle digital, fly by wire, flight control system presents an interesting challenge in avionics system design. In residence in each of four redundant general purpose computers at lift off are the guidance, navigation, and control algorithms for the entire flight. The mission is divided into several flight segments: first stage ascent, second stage ascent; abort to launch site, abort once around; on orbit operations, entry, terminal area energy management; and approach and landing. The FCS is complicated in that it must perform the functions to fly the shuttle as a boost vehicle, as a spacecraft, as a reentry vehicle, and as a conventional aircraft. The crew is provided with both manual and automatic modes of operations in all flight phases including touchdown and rollout.
Document ID
19760024058
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Minott, G. M.
(Rockwell Intern. Corp. Houston, TX, United States)
Peller, J. B.
(Rockwell Intern. Corp.)
Cox, K. J.
(NASA Lyndon B. Johnson Space Center)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Publication Information
Publication: Advanced Control Technol. and its Potential for Future Transport Aircraft
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
76N31146
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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