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Parameter estimation of large flexible aerospace structures with application to the control of the Maypole Deployable Reflector

Author:
Balas, M. J.
Published:
Nov 6, 1981.
Physical Description:
1 electronic document
Online Version

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Summary:
Systems such as the Maypole deployable reflector have a distributed parameter nature. The flexible column and hoop structure and the circular antenna of 30-100 meter diameter which it supports are described by partial, rather than ordinary, differential equations. Progress completed in reduced order modelling andd controller design and digital parameter estimation and control is summarized. Topics covered include depolyment and on-orbit operation; quasi-static (steady state) operation; dynamic distributed parameter system; autoregressive moving average identification; frequency domain procedures; direct or implicit active control; adaptive observers; parameter estimation using a linear reinforcement learning factor; feedback control; and reduced order modeling for nonlinear systems.
Other Subject(s):
Collection:
NASA Technical Reports Server (NTRS) Collection.
Note:
Document ID: 19820003226.
Accession ID: 82N11099.
NASA-CR-164971.
Terms of Use and Reproduction:
No Copyright.
View MARC record | catkey: 15717746