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Design of automatic carrier landing system using H control

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2 Author(s)
Suozhong Yuan ; Nanjing Univ. of Aeronaut. & Astronaut., China ; Yidong Yang

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

Published in:

Intelligent Control and Automation, 2000. Proceedings of the 3rd World Congress on  (Volume:5 )

Date of Conference: