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Shuttle orbit flight control design lessons - Direction for Space StationThe Space Shuttle orbit flight control system, which operates during all exo-atmospheric flight phases, has successfully met operational requirements. Many design integration and operational issues that required resolution during development and testing provide an experience base that will benefit the development of future space systems, particularly the Space Station. To this end, the applicable Shuttle and Space Station hardware/software is reviewed with some perspective provided on how current design groundrules were derived and how issues that affected the Shuttle orbit control system design are a pathway for the Space Station. Some of the most significant lessons learned from the Shuttle are summarized, with a discussion of the effect of performance and design of hardware, including the data processing system on software structures and usage procedures. Crew interface issues and important results from man-in-the-loop tests are summarized. Problems resulting from trying to meet difficult orbital operational objectives, including some sophisticated payload operations are characterized. Several proposed Shuttle flight control design improvements, developed in response to some of the lessons learned so far, are identified. Potential application of the Shuttle design lessons and new control technologies to the Space Station are discussed.
Document ID
19870050021
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Cox, Kenneth J.
(NASA Johnson Space Center Houston, TX, United States)
Hattis, Philip D.
(Charles Stark Draper Laboratory, Inc. Cambridge, MA, United States)
Date Acquired
August 13, 2013
Publication Date
March 1, 1987
Publication Information
Publication: IEEE, Proceedings
Volume: 75
ISSN: 0018-9219
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87A37295
Funding Number(s)
CONTRACT_GRANT: NAS9-17560
Distribution Limits
Public
Copyright
Other

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