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The control and estimation of large space structuresA shape control or estimation problem for a large space structure can be modeled by a partial differential equation which represents changes in shape with respect to space and time, together with spatially discrete forcing functions or observations which represent the placement of actuators or sensors at discrete points along the structure. The use of Green's functions to convert boundary value problems into integral equations provides a convenient treatment of this mixture of continuous and discrete mathematics. Control and estimation algorithms are developed for the one-dimensional static beam to illustrate this technique.
Document ID
19810061144
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Weeks, C.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: Joint Automatic Control Conference
Location: San Francisco, CA
Start Date: August 13, 1980
End Date: August 15, 1980
Accession Number
81A45548
Distribution Limits
Public
Copyright
Other

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