Title :
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
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;
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
DOI :
10.1109/IFITA.2010.336