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Flexible structure control laboratory development and technology demonstrationAn experimental structure is described which was constructed to demonstrate and validate recent emerging technologies in the active control and identification of large flexible space structures. The configuration consists of a large, 20 foot diameter antenna-like flexible structure in the horizontal plane with a gimballed central hub, a flexible feed-boom assembly hanging from the hub, and 12 flexible ribs radiating outward. Fourteen electrodynamic force actuators mounted to the hub and to the individual ribs provide the means to excite the structure and exert control forces. Thirty permanently mounted sensors, including optical encoders and analog induction devices provide measurements of structural response at widely distributed points. An experimental remote optical sensor provides sixteen additional sensing channels. A computer samples the sensors, computes the control updates and sends commands to the actuators in real time, while simultaneously displaying selected outputs on a graphics terminal and saving them in memory. Several control experiments were conducted thus far and are documented. These include implementation of distributed parameter system control, model reference adaptive control, and static shape control. These experiments have demonstrated the successful implementation of state-of-the-art control approaches using actual hardware.
Document ID
19890010780
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Vivian, H. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Blaire, P. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Eldred, D. B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Fleischer, G. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ih, C.-H. C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Nerheim, N. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Scheid, R. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wen, J. T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Subject Category
Aircraft Stability And Control
Report/Patent Number
JPL-PUBL-88-29
NASA-CR-184867
NAS 1.26:184867
Report Number: JPL-PUBL-88-29
Report Number: NASA-CR-184867
Report Number: NAS 1.26:184867
Accession Number
89N20151
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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