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Volumn 214, Issue 1, 2000, Pages 1-8

Aircraft pitch and heave rate control

Author keywords

Aircraft; Control; Feedback; Heave; Pitch

Indexed keywords

AERODYNAMICS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; FEEDBACK CONTROL; TRANSIENTS;

EID: 0006174591     PISSN: 09544100     EISSN: None     Source Type: Journal    
DOI: 10.1243/0954410001531872     Document Type: Article
Times cited : (3)

References (14)
  • 5
    • 0023400876 scopus 로고
    • Solution of the Grumman F-14 benchmark control problem
    • August
    • Rimer, M. and Frederick, D. K. Solution of the Grumman F-14 benchmark control problem. IEEE Control Syst., August 1987, 30-40.
    • (1987) IEEE Control Syst. , pp. 30-40
    • Rimer, M.1    Frederick, D.K.2
  • 8
    • 0024889713 scopus 로고
    • Grumman F-14 benchmark control problem solution using BLRLAB
    • Tampa, Florida
    • Milne, G. W. Grumman F-14 benchmark control problem solution using BLRLAB. In Proceedings of IEEE Control Systems Design Workshop, Tampa, Florida, 1989, pp. 94-101.
    • (1989) Proceedings of IEEE Control Systems Design Workshop , pp. 94-101
    • Milne, G.W.1
  • 9
    • 0003638367 scopus 로고
    • Digital control of highly augmented combat aircraft
    • May
    • Tischler, M. B. Digital control of highly augmented combat aircraft. NASATM 88346, May 1987.
    • (1987) NASATM 88346
    • Tischler, M.B.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.