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Volumn 37, Issue 8, 2006, Pages 585-597

Polynomial approach for design and robust analysis of Lateral missile control

Author keywords

Eigenstructure assignment; Finite Inclusion Theorem; Finite Nyquist Theorem; Kharitonov; Linear parameter varying systems; Missile autopilot; Robust control

Indexed keywords

CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL EQUIPMENT; EIGENVALUES AND EIGENFUNCTIONS; MATRIX ALGEBRA; POLYNOMIALS; THEOREM PROVING;

EID: 33745700102     PISSN: 00207721     EISSN: 14645319     Source Type: Journal    
DOI: 10.1080/00207720600784742     Document Type: Conference Paper
Times cited : (6)

References (25)
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    • Kaminsky, R.D.1    Djaferis, T.E.2
  • 19
    • 0035279041 scopus 로고    scopus 로고
    • Robust design of sideslip velocity autopilot for a quasi-linear parameter-varying missile model
    • A. Tsourdos, R. Zbikowski and B.A. White, "Robust design of sideslip velocity autopilot for a quasi-linear parameter-varying missile model", Journal of Guidance, Control, and Dynamics, 24(2), pp. 287-295, 2001.
    • (2001) Journal of Guidance, Control, and Dynamics , vol.24 , Issue.2 , pp. 287-295
    • Tsourdos, A.1    Zbikowski, R.2    White, B.A.3
  • 20
  • 22
    • 0030706453 scopus 로고    scopus 로고
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    • B.A. White, "Robust polynomial eigenstructure assignment using dynamic feedback controllers", IMechE, Systems and Control Engineering, 211(11), pp. 35-51, 1997.
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  • 24
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    • Missile autopilot robustness to uncertain aerodynamics: Stability hypersphere radius calculation
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  • 25
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    • Comparison of 6 robustness tests evaluating missile autopilot robustness to uncertain aerodynamics
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.