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Control Augmented Structural SynthesisA methodology for control augmented structural synthesis is proposed for a class of structures which can be modeled as an assemblage of frame and/or truss elements. It is assumed that both the plant (structure) and the active control system dynamics can be adequately represented with a linear model. The structural sizing variables, active control system feedback gains and nonstructural lumped masses are treated simultaneously as independent design variables. Design constraints are imposed on static and dynamic displacements, static stresses, actuator forces and natural frequencies to ensure acceptable system behavior. Multiple static and dynamic loading conditions are considered. Side constraints imposed on the design variables protect against the generation of unrealizable designs. While the proposed approach is fundamentally more general, here the methodology is developed and demonstrated for the case where: (1) the dynamic loading is harmonic and thus the steady state response is of primary interest; (2) direct output feedback is used for the control system model; and (3) the actuators and sensors are collocated.
Document ID
19880010906
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Lust, Robert V.
(California Univ. Los Angeles, CA, United States)
Schmit, Lucien A.
(California Univ. Los Angeles, CA, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1988
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-4132
NAS 1.26:4132
Report Number: NASA-CR-4132
Report Number: NAS 1.26:4132
Accession Number
88N20290
Funding Number(s)
PROJECT: RTOP 505-63-11-01
CONTRACT_GRANT: NSG-1490
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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