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Volumn 251, Issue 3, 2002, Pages 543-557

Acceleration-based vibration control of distributed parameter systems using the "reciprocal state-space framework"

Author keywords

[No Author keywords available]

Indexed keywords

ACCELERATION; CONTROL SYSTEM SYNTHESIS; DISTRIBUTED PARAMETER CONTROL SYSTEMS; FEEDBACK CONTROL; STATE SPACE METHODS;

EID: 0037187974     PISSN: 0022460X     EISSN: None     Source Type: Journal    
DOI: 10.1006/jsvi.2001.3842     Document Type: Editorial
Times cited : (38)

References (25)
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  • 7
    • 0030107374 scopus 로고    scopus 로고
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    • P. J. Veitch et al. 1996 Review of Scientific Instruments 67, (Part 1), 633-640. Can piezoelectric accelerometers be used to actively damp the mechanical suspensions in laser interferometric gravitational wave detectors.
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    • Veitch, P.J.1
  • 9
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    • Control design of linear dynamic system with matrix differential equations for equations for aerospace applications
    • Ph.D. Dissertation, Department of Aerospace Engineering, The Ohio State University, Columbus
    • Y.-W. Tseng and R. K. Yedavalli 1997 Ph.D. Dissertation, Department of Aerospace Engineering, The Ohio State University, Columbus. Control design of linear dynamic system with matrix differential equations for equations for aerospace applications.
    • (1997)
    • Tseng, Y.-W.1    Yedavalli, R.K.2
  • 10
    • 84959111186 scopus 로고    scopus 로고
    • New modeling and control design techniques for smart deformable aircraft structures with acceleration feedback
    • Portland, OR, U.S.A.
    • S. K. Kwak and R. K. Yedavalli 1999 Guidance, Navigation, and Control Conference, 1686-1696. Portland, OR, U.S.A. New modeling and control design techniques for smart deformable aircraft structures with acceleration feedback.
    • (1999) Guidance, Navigation, and Control Conference , pp. 1686-1696
    • Kwak, S.K.1    Yedavalli, R.K.2
  • 15
    • 0003906107 scopus 로고    scopus 로고
    • New modeling and control design techniques for aircraft structural dynamics using smart materials
    • Ph.D. Dissertation, Department of Aerospace Engineering, The Ohio State University, Columbus
    • S.-K. Kwak and R. K. Yedavalli 1999 Ph.D. Dissertation, Department of Aerospace Engineering, The Ohio State University, Columbus. New modeling and control design techniques for aircraft structural dynamics using smart materials.
    • (1999)
    • Kwak, S.-K.1    Yedavalli, R.K.2
  • 17
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    • Controllability and observability of linear matrix-second-order system
    • P. C. Hughes and R. E. Skelton 1980 Journal of Applied Mechanics 47, 415-420. Controllability and observability of linear matrix-second-order system.
    • (1980) Journal of Applied Mechanics , vol.47 , pp. 415-420
    • Hughes, P.C.1    Skelton, R.E.2
  • 18
    • 0004163205 scopus 로고
    • New York: John Wiley & Sons, Inc.; second edition
    • F. L. Lewis and V. L. Syrmos 1995 Optimal Control. New York: John Wiley & Sons, Inc.; second edition.
    • (1995) Optimal Control
    • Lewis, F.L.1    Syrmos, V.L.2
  • 21
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    • Kirk, D.E.1
  • 23
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    • Distributed piezoelectric-polymer active vibration control of a cantilever beam
    • T. Bailey and J. E. Hubbard 1985 Journal of Guidance and Control 8, 605-611. Distributed piezoelectric-polymer active vibration control of a cantilever beam.
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  • 24
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    • Induced strain actuation of composite beam and rotor blades with embedded piezoceramic elements
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    • (1996) Smart Structures and Materials , vol.5 , pp. 35-48
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.