DECOUPLING CONTROL LAW DESIGN FOR OBLIQUE-WING AIRCRAFT BASED ON EIGENSTRUCTURE ASSIGNMENT AND MODEL FOLLOWING
International Council of the Aeronautical Sciences
2021-01-01
9 pages
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
The Decoupling Design of Aircraft Lateral Flight Control Systems with Eigenstructure Assignment
British Library Conference Proceedings | 1994
|Eigenstructure synthesis of an oblique wing flight control system
Tema Archive | 1985
|Lateral Directional Aircraft Control Using Eigenstructure Assignment
Online Contents | 1998
|Eigenstructure Assignment for a Tailless Aircraft
AIAA | 2007
|