Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Liuli Ou"'
Publikováno v:
Journal of Applied Mathematics, Vol 2014 (2014)
To validate the robust stability of the flight control system of hypersonic flight vehicle, which suffers from a large number of parametrical uncertainties, a new clearance framework based on structural singular value (μ) theory and global uncertain
Externí odkaz:
https://doaj.org/article/34b136ce1dfd4078935418ded09bbb74
Publikováno v:
Journal of Control Science and Engineering, Vol 2014 (2014)
A new approach for pole placement of single-input system is proposed in this paper. Noncritical closed loop poles can be placed arbitrarily in a specified convex region when dominant poles are fixed in anticipant locations. The convex region is expre
Externí odkaz:
https://doaj.org/article/1560818083ec4df59c6a9df5ca169713
Publikováno v:
IEEE Transactions on Aerospace and Electronic Systems. 51:2138-2147
This paper studies the clearance of flight control law for a hypersonic gliding vehicle (HGV) and proposes two linear clearance criteria based on structural singular value (μ) theory. The first criterion is the multiinput-multioutput (MIMO) stabilit
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering. 229:506-516
This article investigates the problem of robust stabilization for a flexible launch vehicle. Since the launch vehicle suffers from parametric uncertainties, bending modes, and external wind disturbances simultaneously, an observer-based methodology i
Publikováno v:
IET Control Theory & Applications. 9:441-446
This study addresses the cooperative control problem of multi-missile systems. It proposed a two-stage control strategy, aiming at simultaneous attack from a group of missiles at a static target. The first stage adopts a special distributed consensus
Publikováno v:
Journal of Applied Mathematics, Vol 2014 (2014)
J. Appl. Math.
J. Appl. Math.
To validate the robust stability of the flight control system of hypersonic flight vehicle, which suffers from a large number of parametrical uncertainties, a new clearance framework based on structural singular value (μ) theory and global uncertain
Publikováno v:
2015 34th Chinese Control Conference (CCC); 2015, p6884-6888, 5p
Publikováno v:
International Journal of Modelling, Identification and Control. 19:290
This paper proposes robust tracking performance criterion for flight control system clearance while other linear methods focus on robust stability criterion or stability margin criterion. The new criterion aims at guarantee of fast and accurate track
Publikováno v:
Proceedings of the 31st Chinese Control Conference; 1/ 1/2012, p3166-3170, 5p