Describes the background to the use of a number of Hinfinity 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 Hinfinity methods and presents conclusions.
Decoupling control of a linear VSTOL model using Hinfinity techniques
Entkopplungsregelung eines linearen VSTOL Modells mit H<sub>Infinität</sub>-Verfahren
IEE Colloquium on 'Navigation, Guidance and Control on Aerospace' ; No.142 ; 6/1-6/10
1989
, 17 Quellen
Aufsatz (Konferenz)
Englisch
VSTOL first flight on an Hinfinity control law
Tema Archiv | 1995
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