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Volumn 4, Issue , 2008, Pages 1515-1526

A simulation benchmark for aircraft survivability assessment

Author keywords

Aircraft survivability; Fault tolerant control; Reconfigurable control

Indexed keywords

AIRCRAFT SURVIVABILITY; DELFT UNIVERSITY OF TECHNOLOGY; FAULT DETECTION AND IDENTIFICATION; FAULT TOLERANT CONTROL; INTELLIGENT FLIGHT CONTROLS; LARGE TRANSPORT AIRCRAFT; RECONFIGURABLE CONTROL; RECONFIGURABLE FLIGHT CONTROL;

EID: 84879008047     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (10)

References (6)
  • 4
    • 52449128042 scopus 로고    scopus 로고
    • SIMONA Flight Simulator Implementation of a Fault Tolerant Sliding Mode Scheme with On-line Control Allocation
    • Proceedings of the American Control Conference, Seattle
    • Alwi H, Edwards C, Stroosma O, and Mulder J.A. SIMONA Flight Simulator Implementation of a Fault Tolerant Sliding Mode Scheme with On-line Control Allocation. Proceedings of the American Control Conference, Seattle, 2008.
    • (2008)
    • Alwi, H.1    Edwards, C.2    Stroosma, O.3    Mulder, J.A.4
  • 5
    • 84879009991 scopus 로고    scopus 로고
    • Flight control reconfiguration based on Online Physical Model Identification and Nonlinear Dynamic Inversion
    • AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA-2008-7435, Honolulu (HI)
    • Lombaerts T.J.J, Huisman H, Chu Q, Mulder J, Joosten D. Flight control reconfiguration based on Online Physical Model Identification and Nonlinear Dynamic Inversion AIAA Guidance, Navigation and Control Conference and Exhibit, AIAA-2008-7435, Honolulu (HI), 2008.
    • (2008)
    • Lombaerts, T.J.J.1    Huisman, H.2    Chu, Q.3    Mulder, J.4    Joosten, D.5


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.