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Volumn 5, Issue 1, 2011, Pages 37-47

Safety-critical design of electromechanical actuation systems in commercial aircraft

Author keywords

[No Author keywords available]

Indexed keywords

COMMERCIAL AIRCRAFT; CONVENTIONAL POWER; CRITICAL DESIGN; ELECTRICAL DRIVES; ELECTRO-MECHANICAL ACTUATOR; ELECTROMECHANICAL ACTUATION; FAULT-TOLERANT; GENERIC DESIGN; MORE ELECTRIC AIRCRAFT; NEW TECHNOLOGIES; SAFETY REQUIREMENTS; SAFETY-CRITICAL;

EID: 79551589207     PISSN: 17518660     EISSN: 17518679     Source Type: Journal    
DOI: 10.1049/iet-epa.2009.0304     Document Type: Article
Times cited : (104)

References (24)
  • 1
    • 79551613160 scopus 로고    scopus 로고
    • 'Advanced secondary power system for transport aircraft', May, 1985
    • 'Advanced secondary power system for transport aircraft', May, 1985
  • 5
    • 0026840181 scopus 로고
    • IEEE Aerosp. Electron. Syst. Mag. Part 1
    • 10.1109/62.141899
    • Sadeghi, T., and Lyons, A.: 'Fault tolerant EHA architectures', IEEE Aerosp. Electron. Syst. Mag. Part 1, 1992, 7, (3), p. 32-4210.1109/62.141899
    • (1992) Fault tolerant EHA architectures , vol.7 , Issue.3 , pp. 32-42
    • Sadeghi, T.1    Lyons, A.2
  • 24
    • 79551594863 scopus 로고    scopus 로고
    • RTCA: 'DO-160F. Environmental conditions and test procedures for airborne equipment'. Aviation industry standards and procedures document, 2007 16-41
    • RTCA: 'DO-160F. Environmental conditions and test procedures for airborne equipment'. Aviation industry standards and procedures document, 2007, pp. 16-41


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.