DocumentCode :
490552
Title :
Arrow Mode Reboost Analysis for Space Station Freedom
Author :
Graham, Ronald E. ; DuFore, Valerie J.
Author_Institution :
Control Systems Branch, NASA Lewis Research Center, 21000 Brookpark Road, Cleveland OH 44135. ecaxron@ariel.lerc.nasa.gov
fYear :
1993
fDate :
2-4 June 1993
Firstpage :
2485
Lastpage :
2489
Abstract :
Early flights of Space Station Freedom are gravity-gradient stabilized, but reboost to higher altitude while in Arrow Mode, where its truss is aligned with the direction of flight. Power concerns led to a proposal to activate Freedom´s solar array beta gimbals for partial sun tracking during reboost. Further plume impingement concerns led to a baseline orientation of flight with the arrays leading. A baseline dynamic simulation for this maneuver is presented here. Several observations are made, particularly about large motions of the beta gimbals during the maneuver, and about simplified structural dynamic response of the arrays to the reboost and large slew environment. The results presented here may be used as a starting point for reboost analyses on other flight configurations, or in other orientations, or with higher-fidelity structural information.
Keywords :
Aerospace engineering; Control systems; Equations; Information analysis; Motion control; NASA; Proposals; Space stations; Sun; Torque;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1993
Conference_Location :
San Francisco, CA, USA
Print_ISBN :
0-7803-0860-3
Type :
conf
Filename :
4793337
Link To Document :
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