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PACOSS program status and resultsFuture large space systems (LSS), both civilian and military, will have performance objectives which require stringent pointing accuracies, relatively fast retargeting times, short settling times, accurate dynamic shape requirements, or combinations thereof. Many of these structures will be large but lightweight and will exhibit a dense, low-frequency modal spectrum with significant content within the control bandwidth. Although it is possible in principle to achieve structural vibration control with purely active means, experience with complex structures has shown that the realities of plant model inaccuracies and real sensor and actuator dynamics frequently combine to produce disappointing results. It was shown that a combination of passive and active control will result in a simpler system which can be expected to be more reliable and less expensive than a corresponding system utilizing active control exclusively. The goals of the Passive and Active Control of Space Structures (PACOSS) program consist of a thorough investigation of the relative roles of passive active vibration control, and the development of validated means of vibration control. The program approach, representative system article, dynamic test article, and test status and results are outlined.
Document ID
19900011749
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Richards, K. E., Jr.
(Martin Marietta Aerospace Denver, CO, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Publication Information
Publication: NASA, Langley Research Center, NASA(DOD Controls-Structure Interaction Technology 1989
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
90N21065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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