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Volumn 338, Issue 2-3, 2001, Pages 133-147

Control of a directly excited structural dynamic model of an F-15 tail section

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; BIFURCATION (MATHEMATICS); BUFFETING; CERAMIC MATERIALS; COMPUTER SIMULATION; DIGITAL CONTROL SYSTEMS; EMPENNAGES; EQUATIONS OF MOTION; FLIGHT DYNAMICS; PERTURBATION TECHNIQUES; PIEZOELECTRIC DEVICES; VIBRATION CONTROL;

EID: 0035276104     PISSN: 00160032     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0016-0032(00)00075-2     Document Type: Article
Times cited : (10)

References (13)
  • 1
    • 0024892973 scopus 로고
    • Some aspects of aircraft dynamic loads due to flow separation
    • Mabey D.G. Some aspects of aircraft dynamic loads due to flow separation. Prog. Aerospace Sci. 26:1989;115-151.
    • (1989) Prog. Aerospace Sci. , vol.26 , pp. 115-151
    • Mabey, D.G.1
  • 12
    • 85031533133 scopus 로고    scopus 로고
    • SIMULINK: Dynamic System Simulation Software
    • Natick, MA
    • SIMULINK: Dynamic System Simulation Software, The MathWorks, Natick, MA.
    • The MathWorks


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.