Design and ground-based simulation of an \(H_\infty\) limited authority flight control system for the Westland Lynx Helicopter (Q2729292)
From MaRDI portal
 | This is the item page for this Wikibase entity, intended for internal use and editing purposes. Please use this page instead for the normal view: Design and ground-based simulation of an \(H_\infty\) limited authority flight control system for the Westland Lynx Helicopter |
scientific article; zbMATH DE number 1621953
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Design and ground-based simulation of an \(H_\infty\) limited authority flight control system for the Westland Lynx Helicopter |
scientific article; zbMATH DE number 1621953 |
Statements
23 September 2001
0 references
control systems
0 references
limited authority
0 references
saturation
0 references
\(H_\infty\) control
0 references
helicopter
0 references
anti-windup compensator
0 references
testing
0 references
piloting simulation
0 references
Design and ground-based simulation of an \(H_\infty\) limited authority flight control system for the Westland Lynx Helicopter (English)
0 references
The limited authority control system is designed for the Westland Lynx Helicopter. The \(H_{\infty}\) method is used for controller synthesis, including the anti-windup compensator design. The control system configuration is described and discussed, and the results from desktop testing and piloting simulation are presented.
0 references
