DocumentCode :
1206242
Title :
Guidance and Control of Missile Interceptor using Second-Order Sliding Modes
Author :
Shtessel, Yuri B. ; Shkolnikov, Ilya A. ; Levant, Arie
Author_Institution :
Electr. & Comput. Eng. Dept., Univ. of Alabama in Huntsville, Huntsville, AL
Volume :
45
Issue :
1
fYear :
2009
Firstpage :
110
Lastpage :
124
Abstract :
A new smooth second-order sliding mode control (SSOSM) is proposed and proved for a system driven by uncertain sufficiently smooth disturbances. The main target application of this technique, the missile interceptor guidance-control system against targets performing evasive maneuvers, is considered to demonstrate benefits of this design for a two-loop integration of guidance and flight control systems. The designed guidance-control system performance is verified via computer simulations using a miniature hypervelocity kinetic energy endo-atmospheric interceptor planar model.
Keywords :
control system synthesis; missile guidance; variable structure systems; evasive maneuvers; flight control systems; guidance control systems; missile interceptor control; missile interceptor guidance; second-order sliding mode control; Aerospace control; Computer simulation; Kinetic energy; Missiles; Navigation; Robust control; Robustness; Sliding mode control; System performance; Uncertainty;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2009.4805267
Filename :
4805267
Link To Document :
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