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Flight Control Overview of STS-88, the First Space Station Assembly FlightWhen the Space Shuttle Endeavour undocked from the Zarya/Unity configuration on STS-88 it marked the completion of the most challenging shuttle mission to date and the beginning of an enormous task of assembling the International Space Station. The flight offered an array of complex dynamics and control related challenges to mate the American module 'Unity' to the Russian module 'Zarya'. Capability demonstrated on the flight included closed-loop thruster control in the presence of low frequency structural dynamics and mated-vehicle translational maneuvers in the presence of structural loads and thruster hardware constraints. The flight was a complete success from all aspects. This paper will give an overview of the flight control challenges encountered and the actual control performance observed for the on-orbit operations. Included will be the shuttle analysis and filtering strategies to ensure control system stability in the presence of low frequency flex-body dynamics.
Document ID
20000085623
Acquisition Source
Johnson Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hall, Robert
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Kirchwey, Kim
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Martin, Michael
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Rosch, Gene
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Zimpfer, Douglas
(Draper (Charles Stark) Lab., Inc. Cambridge, MA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 1999
Subject Category
Space Transportation And Safety
Funding Number(s)
CONTRACT_GRANT: NAS9-19556
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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