메뉴 건너뛰기




Volumn 11, Issue 5, 2003, Pages 551-558

Design and flight test of a robust autopilot for the IRIS-T air-to-air missile

Author keywords

Flight control; Flight test; H infinity control; Missiles; Robust control

Indexed keywords

ACTUATORS; AERODYNAMICS; AUTOMATIC PILOTS; BANDWIDTH; COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); FLIGHT DYNAMICS; INFRARED IMAGING; MANEUVERABILITY; MILITARY OPERATIONS; ROBUSTNESS (CONTROL SYSTEMS); TIME VARYING CONTROL SYSTEMS;

EID: 0037403389     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(02)00063-1     Document Type: Article
Times cited : (50)

References (11)
  • 1
    • 0032785313 scopus 로고    scopus 로고
    • Full envelope missile autopilot design using gain scheduled robust control
    • Buschek, H. (1999). Full envelope missile autopilot design using gain scheduled robust control. Journal of Guidance, Control, and Dynamics, 22(1), 115-122.
    • (1999) Journal of Guidance, Control, and Dynamics , vol.22 , Issue.1 , pp. 115-122
    • Buschek, H.1
  • 4
    • 0003542268 scopus 로고
    • ∞ Aerospace control design: A VSTOL flight application
    • London: Springer
    • ∞ Aerospace control design: A VSTOL flight application. Advances in industrial control series. London: Springer.
    • (1995) Advances in Industrial Control Series
    • Hyde, R.A.1
  • 7
    • 0027205718 scopus 로고
    • The complex structured singular value
    • Packard, A., & Doyle, J. C. (1993). The complex structured singular value. Automatica, 29(1), 71-109.
    • (1993) Automatica , vol.29 , Issue.1 , pp. 71-109
    • Packard, A.1    Doyle, J.C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.