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Proof-mass actuator placement strategies for regulation of flexure during the SCOLE slewAn analysis was performed in order to find the best placement for proof-mass actuators and to determine the importance of placement, i.e., what is the sensitivity of beam flexure to actuator placement. The analysis was performed by using the NASTRAN finite element model for a flexible beam with 21 grid points on beam, by using the nonlinear DISCOS simulation of 20 deg slew and the use of a closed-loop linear quadratic regulator (lqr). Some conclusions reached are: (1) proof-mass actuators can reduce flexure amplitude and damp oscillations; (2) amplitude of deformations during slew is relatively insensitive to placement of actuators; (3) damping factor of oscillations is sensitive to actuator placement; and (4) the degree of controllability method indicates most effective placement for actuators.
Document ID
19870008397
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Fisher, Shalom (mike)
(Naval Research Lab., Washington, DC, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Langley Research Center Proceedings of the 3rd Annual SCOLE Workshop
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
87N17830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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