A Kind of Discrete Variable Structure UCAV Guidance Law Restrict by the Entering Angle

Author

Zhaoqiang, Li ; Deyun, Zhou ; Jiadong, Xu

Author_Institution

Dept. of Electron. Inf., Northwestern Polytech. Univ., Xian, China

Volume

3

fYear

2010

fDate

16-18 July 2010

Firstpage

237

Lastpage

240

Abstract

To solve the problem that the UCAV load data link make analog signals guidance law cannot be used directly, a kind of new discrete variable structure guidance law arithmetic is brought out, which takes the restriction of entry angle into consideration, and conquers the buffeting phenomenon when the tradition discrete variable structure control arithmetic get into sliding mode. The simulation results show that the discrete signal guidance law can meet the tactical UCAV indicator.

Keywords

aircraft; aircraft landing guidance; mobile robots; remotely operated vehicles; variable structure systems; UCA V load data link; analog signal guidance law; buffeting phenomenon; discrete variable structure UCAV guidance law; entering angle; sliding mode control; Control systems; Equations; Mathematical model; Prediction algorithms; Radar tracking; Robustness; Target tracking; discrete signal; guidance law; no buffeting; the restriction of entry angle; variable structure control;

fLanguage

English

Publisher

ieee

Conference_Titel

Information Technology and Applications (IFITA), 2010 International Forum on

Conference_Location

Kunming

Print_ISBN

978-1-4244-7621-3

Electronic_ISBN

978-1-4244-7622-0

Type

conf

DOI

10.1109/IFITA.2010.336

Filename

5634654