Article ID Journal Published Year Pages File Type
708038 European Journal of Control 2006 15 Pages PDF
Abstract

In this paper, a complete methodology is detailed for the design and analysis of robust gain-scheduled fighter aircraft flight control laws. The proposed approach consists of three steps. A set of locally robust controllers is first generated using LMI optimization. The global controller is then obtained by a standard linear interpolation and transformed into LFT format. Finally, a validation step is achieved using both LTI and LTVan alysis techniques, for which specific methods and tools have been developed.

Related Topics
Physical Sciences and Engineering Engineering Control and Systems Engineering