Title :
Design of automatic carrier landing system using H∞ control
Author :
Suozhong, Yuan ; Yidong, Yang
Author_Institution :
Nanjing Univ. of Aeronaut. & Astronaut., China
Abstract :
In this paper, the design of an automatic carrier landing system (ACLS) is accomplished using H-infinity techniques, in which the single input/output design specifications were translated into the weighting functions of the H-infinity synthesis problem. The objective of the design is to improve the ACLS´s path precision under the worst-case condition of a vertical gust during carrier landing. The design yields a satisfactory response
Keywords :
H∞ control; aircraft control; aircraft landing guidance; control system synthesis; marine systems; naval engineering computing; wind; H∞ control; H∞ synthesis problem; aircraft carriers; automatic carrier landing system design; flight control; input/output design specifications; path precision; vertical gust; weighting functions; worst-case condition; Automatic control; Control systems;
Conference_Titel :
Intelligent Control and Automation, 2000. Proceedings of the 3rd World Congress on
Conference_Location :
Hefei
Print_ISBN :
0-7803-5995-X
DOI :
10.1109/WCICA.2000.863180
