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Volumn 73, Issue 1, 2001, Pages 16-25

Design of robust autopilot-output integral sliding mode controllers for guided missile systems with parameter perturbations

Author keywords

Aircraft; Autopilots; Controllers; Guided missile systems

Indexed keywords

AIRCRAFT; COMPUTER SIMULATION; LYAPUNOV METHODS; ROBUSTNESS (CONTROL SYSTEMS); SLIDING MODE CONTROL;

EID: 0035780886     PISSN: 00022667     EISSN: None     Source Type: Journal    
DOI: 10.1108/00022660110366854     Document Type: Article
Times cited : (14)

References (14)
  • 9
    • 0034291385 scopus 로고    scopus 로고
    • Robust sliding mode flight control systems for the uncertain MIMO aircraft model F-18
    • Jafarov, E.M. and Tasaltin, R. (2000), "Robust sliding mode flight control systems for the uncertain MIMO aircraft model F-18", Transactions on Aerospace and Electronic Systems, Vol. 36 No. 4 (10), pp. 1-15.
    • (2000) Transactions on Aerospace and Electronic Systems , vol.36 , Issue.4-10 , pp. 1-15
    • Jafarov, E.M.1    Tasaltin, R.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.