In this paper, a flight control law for a simplified F-14 aircraft model is designed based on variable structure control (VSC) theory. For m-input, q-output linear uncertain systems (q
Variable structure robust flight control system for the F-14
IEEE Transactions on Aerospace and Electronic Systems ; 33 , 1 ; 77-84
1997-01-01
1489869 byte
Article (Journal)
Electronic Resource
English
Variable Structure Robust Flight Control System for the F-14
Online Contents | 1997
|Robust Variable Structure Controller Design for Fault Tolerant Flight Control
British Library Conference Proceedings | 1998
|