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Volumn 5, Issue , 2002, Pages 3637-3643

MIMO sliding mode control as an alternative to reconfigurable flight control designs

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AVIATION; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; FREQUENCY DOMAIN ANALYSIS; MATHEMATICAL MODELS; OBSERVABILITY; SENSITIVITY ANALYSIS;

EID: 0036061011     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2002.1024493     Document Type: Conference Paper
Times cited : (8)

References (17)
  • 2
    • 0032021448 scopus 로고    scopus 로고
    • Robust exact differentiation via sliding mode technique
    • (1998) Automatica , vol.34 , Issue.3 , pp. 379-384
    • Levant, A.1
  • 14
    • 4243643652 scopus 로고    scopus 로고
    • Application of sliding mode methods to the design of reconfigurable flight control systems
    • Ph.D. Dissertation, Dept. of Mechanical and Aeronautical Engineering, University of California, Davis
    • (2002)
    • Wells, S.R.1
  • 15
    • 4243714673 scopus 로고    scopus 로고
    • Multi-input, multi-output flight control design using pseudo control, software rate limiters, and quantitative feedback theory
    • PhD dissertation, Dept. of Mechanical and Aeronautical Engineering, University of California, Davis
    • (1996)
    • Henderson, D.K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.