The guidance system of anti-radiation aircraft

Author

Zhou, Taoyun ; Cheng, Yun ; Zhang, Yi

Author_Institution

Dept. of Commun. & Control Eng., Hunan Inst. of Humanities, Sci. & Technol., Loudi, China

Volume

1

fYear

2008

fDate

17-19 Nov. 2008

Firstpage

1352

Lastpage

1356

Abstract

This paper introduced the characteristics of anti-radiation aircraft and the composition of its guidance system. Based on the aerodynamic parameters and actual flight data of a certain type of airplane, this paper established a mathematical model of direct lateral force control, and put forward a decoupling method for the system. The system employer a tracking method in the guidance of the aircraft and gave simulation results. The advantages of this system are quick response, high percentage of hits, strong wind-resistance ability and casualty effect.

Keywords

aircraft control; force control; aerodynamic parameters; anti-radiation aircraft; casualty effect; direct lateral force control; guidance system; mathematical model; quick response; tracking method; wind-resistance ability; Aerospace control; Aerospace electronics; Airborne radar; Aircraft propulsion; Force control; Intelligent systems; Knowledge engineering; Missiles; Radar detection; Radar tracking; anti-radiation aircraft; direct lateral force control; guidance law; tracking method;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent System and Knowledge Engineering, 2008. ISKE 2008. 3rd International Conference on

Conference_Location

Xiamen

Print_ISBN

978-1-4244-2196-1

Electronic_ISBN

978-1-4244-2197-8

Type

conf

DOI

10.1109/ISKE.2008.4731142

Filename

4731142