Active vibration suppression of a flexible structure using smart material and a modular control patch

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Volumn 214, Issue 4, 2000, Pages 217-229

  Song, G ^a   Schmidt, S P ^a,b   Agrawal, B N ^a,b  

^a The University of Akron   (United States)

^b NAVAL POSTGRADUATE SCHOOL   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; ALGORITHMS; CANTILEVER BEAMS; CONTROL SYSTEM SYNTHESIS; DIGITAL CONTROL SYSTEMS; FEEDBACK CONTROL; INTELLIGENT MATERIALS; PIEZOELECTRIC DEVICES; REAL TIME SYSTEMS; SENSORS; STRAIN RATE; VIBRATION CONTROL;

MINIATURIZED DIGITAL CONTROLLER; MODULAR CONTROL PATCH; POSITIVE POSITION FEEDBACK CONTROL; STRAIN RATE FEEDBACK CONTROL;

FLEXIBLE STRUCTURES;

EID: 0034479956     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/0954410001532024     Document Type: Article

References (7)

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2. Chaudhry, Z. and Rogers, C. Actuators for smart structures. In Fiber Optic Smart Structures, 1995 (John Wiley, New York).
3. Fanson, J. L. and Caughey, T. K. Positive position feedback control for large space structure. Am. Inst. Aeronaut. Astronaut. J., April 1990, 28(4), 717-724.
4. Agrawal, B. N., Bang, H. and Jones, E. Application of piezo- electric actuators and sensors in the vibration control of flexible spacecraft structures. In 43rd Congress of the International Astronautical Federation, Washington, D.C., September 1992.
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6. Bronowicki, A. J. and Rohleen E. Modular control patch (MCP). Final Report, TRW Space and Electronics Group, Redondo Beach, California.
7. TMS320C3x, User's Guide, 1992 (Texas Instruments, Inc.).