Title :
Decoupling control of a linear VSTOL model using H∞ techniques
Author_Institution :
Cambridge Univ., UK
Abstract :
Describes the background to the use of a number of H∞ methods in the design of a decoupled control system for a VSTOL aircraft at an operating point of 120 knots. The author focuses on robustness of multivariable control designs and explains the criteria by which the robustness of designs is assessed. The author discusses the application of various H∞ methods and presents conclusions
Keywords :
aircraft control; control system synthesis; multivariable control systems; stability; H∞ techniques; VSTOL aircraft; aircraft control; control system synthesis; decoupled control system; multivariable control designs; multivariable control systems; robustness;
Conference_Titel :
Navigation, Guidance and Control on Aerospace, IEE Colloquium on
Conference_Location :
London
