DocumentCode :
1765950
Title :
Impact angle constrained sliding mode guidance against maneuvering target with unknown acceleration
Author :
Dongsoo Cho ; Kim, H. Jin ; Min-jea Tahk
Author_Institution :
Dept. of Mech. & Aerosp. Eng., Seoul Nat. Univ., Seoul, South Korea
Volume :
51
Issue :
2
fYear :
2015
fDate :
42095
Firstpage :
1310
Lastpage :
1323
Abstract :
In this paper, a sliding mode guidance law for impact angle control is proposed against a maneuvering target with unknown acceleration, which is capable of achieving the acceptable miss distance and a wide range of the desired impact angle. The main idea is to separate the switching surfaces for the impact angle constraint and the homing constraint, then to associate the two surfaces by introducing an appropriate virtual controller. Because of the unknown target acceleration, an adaptive procedure is designed to select the gain of the switching controller which accounts for the uncertainty bound regarding the target acceleration. The stability of the proposed approach is analyzed by Lyapunov theory, and the capturability analysis is also presented. Simulation results confirm the effectiveness of the proposed guidance against a maneuvering target as well as a nonmaneuvering target with absence and presence of noise.
Keywords :
Lyapunov methods; ships; stability; switching systems (control); variable structure systems; Lyapunov theory; acceptable miss distance; capturability analysis; desired impact angle; homing constraint; impact angle constrained sliding mode guidance; impact angle constraint; impact angle control; maneuvering target; sliding mode guidance law; stability; switching controller; switching surfaces; target acceleration; unknown acceleration; virtual controller; Acceleration; Geometry; Missiles; Stability analysis; Switches; Uncertainty;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/TAES.2015.140358
Filename :
7126185
Link To Document :
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