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Limiting vibration in systems with constant amplitude actuators through command preshapingThe basic concepts of command preshaping were taken and adapted to the framework of systems with constant amplitude (on-off) actuators. In this context, pulse sequences were developed which help to attenuate vibration in flexible systems with high robustness to errors in frequency identification. Sequences containing impulses of different magnitudes were approximated by sequences containing pulses of different durations. The effects of variation in pulse width on this approximation were examined. Sequences capable of minimizing loads induced in flexible systems during execution of commands were also investigated. The usefulness of these techniques in real-world situations was verified by application to a high fidelity simulation of the space shuttle. Results showed that constant amplitude preshaping techniques offer a substantial improvement in vibration reduction over both the standard and upgraded shuttle control methods and may be mission enabling for use of the shuttle with extremely massive payloads.
Document ID
19940028401
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Rogers, Keith Eric
(Draper (Charles Stark) Lab., Inc. Cambridge, MA, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1994
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-188284
NAS 1.26:188284
CSDL-T-1214
Report Number: NASA-CR-188284
Report Number: NAS 1.26:188284
Report Number: CSDL-T-1214
Accession Number
94N32907
Funding Number(s)
CONTRACT_GRANT: NAS9-18426
Distribution Limits
Public
Copyright
Public Use Permitted.
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