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LaRC controls activity for LSSTMath models were developed for various types of large flexible structures. These models were used to study the uncontrolled dynamic characteristics of the structures in orbit and to devise control concepts in order to control their orientation and geometrical shape. Reduced order decoupled control of the 100 meter long free free beam were studied. The inplane orientation and shape of the beam was controlled in a decoupled manner with as few actuators as possible. Using two controllers, near each end of the beam, to produce a 0.01 radian pitch change, perfect decoupled control was achieved for the rigid body pitch theta mode and the first flexible mode A sub 1.
Document ID
19800010888
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Montgomery, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 10, 2013
Publication Date
February 1, 1980
Publication Information
Publication: Large Space Systems Technol., 1979
Subject Category
Launch Vehicles And Space Vehicles
Accession Number
80N19165
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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