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Volumn 24, Issue 4, 2001, Pages 805-815

New modeling and control design techniques for smart deformable aircraft structures

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AERODYNAMIC LOADS; ALGORITHMS; ELECTRIC POTENTIAL; FINITE ELEMENT METHOD; MANEUVERABILITY; MATHEMATICAL MODELS; PIEZOELECTRIC MATERIALS; SENSORS; STATE SPACE METHODS; STIFFNESS MATRIX; WINGS;

EID: 0035393457     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4782     Document Type: Article
Times cited : (18)

References (34)
  • 13
    • 0004005538 scopus 로고    scopus 로고
    • Control design of linear dynamic system with matrix differential equations for equations for aerospace applications
    • Ph.D. Dissertation, Dept. of Aerospace Engineering, The Ohio State Univ., Columbus, OH, Dec.
    • (1997)
    • Tseng, Y.-W.1    Yedavalli, R.K.2
  • 14
    • 0004235689 scopus 로고    scopus 로고
    • Feasibility assessment and optimization study of smart actuation systems for enhanced aircraft maneuver performance
    • Preprint
    • (1997)
    • Appa, K.1    Khot, N.S.2
  • 18
    • 0003167467 scopus 로고
    • Piezoelectric laminates: Theory and experiment for distributed sensors and actuators
    • edited by H. S. Tzou, Kluwer Academic, Boston
    • (1992) Intelligent Structural Systems , pp. 75-167
    • Lee, C.K.1
  • 19
    • 0003906107 scopus 로고    scopus 로고
    • New modeling and control design techniques for aircraft structural dynamics using smart materials
    • Ph.D. Dissertation, Dept. of Aerospace Engineering, The Ohio State Univ., Columbus, OH, June
    • (1999)
    • Kwak, S.K.1    Yedavalli, R.K.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.