作者: Jean-Marc Biannic , C. Roos , A. Knauf
DOI: 10.3166/EJC.12.71-85
关键词:
摘要: 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 three steps. A set locally controllers first generated using LMI optimization. global controller then obtained by standard linear interpolation transformed into LFT format. Finally, validation step achieved both LTI LTV techniques, which specific methods tools have been developed.