Design of Automatic Carrier Landing Control System using Block Diagonal Controller

Author

Zhao, Guorong ; Li, Jixin ; Chen, Muqing

Author_Institution

Dept. of Control Eng., Naval Aeronaut. Eng. Inst., Yantai

Volume

1

fYear

0

fDate

0-0 0

Firstpage

2291

Lastpage

2294

Abstract

The block diagonal controller (BDC) was introduced and the properties of aircraft were analyzed simply. Then, the longitudinal motion equations of aircraft were transformed in block diagonal form. And the inverse-analytic solution of longitudinal motion equations was given. In order to make the aircraft land on carrier precisely, the BDC was used to design the longitudinal automatic carrier landing control system. The mathematical simulation shows that the BDC has achieved the performance specifications of the design and the robustness is also good

Keywords

aircraft landing guidance; motion control; aircraft longitudinal motion equation; aircraft precise landing; aircraft property analysis; automatic carrier landing control; block diagonal controller; inverse-analytic solution; mathematical simulation; Aerospace control; Aerospace engineering; Aircraft propulsion; Automatic control; Control engineering; Control systems; Equations; Military aircraft; Nonlinear control systems; Robustness; automatic carrier landing; block diagonal controller; simulation;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on

Conference_Location

Dalian

Print_ISBN

1-4244-0332-4

Type

conf

DOI

10.1109/WCICA.2006.1712768

Filename

1712768