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Citation: Mc. Turner et I. Postlethwaite, Guaranteed stability regions of linear systems with actuator saturation using the low-and-high gain technique, INT J CONTR, 74(14), 2001, pp. 1425-1434
Citation: Sl. Gatley et al., A partitioned integrated flight and propulsion control system with engine safety limiting, CON ENG PR, 8(8), 2000, pp. 845-859
Citation: E. Prempain et I. Postlethwaite, A new two-degree-of-freedom gain scheduling method applied to the Lynx MK7, P I MEC E I, 214(14), 2000, pp. 299-311
Authors:
Postlethwaite, I
Konstantopoulos, IK
Sun, XD
Walker, DJ
Alford, AG
Citation: I. Postlethwaite et al., Design, flight simulation, and handling qualities evaluation of an LPV gain-scheduled helicopter flight control system, EUR J CONTR, 6(6), 2000, pp. 553-566
Citation: I. Postlethwaite et Dg. Bates, Robust integrated flight and propulsion controller for the Harrier aircraft, J GUID CON, 22(2), 1999, pp. 286-290
Citation: I. Postlethwaite et A. Bartoszewicz, Application of non-linear H-infinity control to the Tetrabot robot manipulator, P I MEC E I, 212(I6), 1998, pp. 459-465