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Volumn 2, Issue , 2007, Pages 1207-1231

Real time damaged aircraft model identification for reconfiguring flight control

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; AERODYNAMICS; AIRCRAFT CONTROL; AIRCRAFT MODELS; COMPUTER SIMULATION; IDENTIFICATION (CONTROL SYSTEMS); AIRCRAFT; FLIGHT CONTROL SYSTEMS; PROJECT MANAGEMENT;

EID: 40549091711     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (38)

References (12)
  • 11
    • 84910146085 scopus 로고    scopus 로고
    • A simulation benchmark for integrated fault tolerant flight control evaluation
    • M.. Smaili, . reeman, ... Lombaerts, and D.A. oosten. A simulation benchmark for integrated fault tolerant flight control evaluation. In AIAA MST, 2 6.
    • AIAA MST , pp. 26
    • Smaili, M.1    Areeman, A.2    Lombaerts, A.3    Loosten, D.A.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.