DocumentCode :
669299
Title :
Robust proportional navigation guidance against highly maneuvering targets
Author :
Seunghyun Kim ; Kim, H.J.
Author_Institution :
Sch. of Mech. & Aerosp. Eng., Seoul Nat. Univ., Seoul, South Korea
fYear :
2013
fDate :
20-23 Oct. 2013
Firstpage :
61
Lastpage :
65
Abstract :
A robust proportional navigation guidance law is proposed by using Lyapunov approach. Proportional navigation guidance(PNG) law is popularly adopted for missile guidance because it is powerful and simple to implement. In fact, it has been shown that PNG is optimal solution for a stationary target. But PNG performance may sharply degrade in the presence of highly maneuvering target. To find estimation of the miss distance, an optimal approach is used. Then switching control is derived by using this estimation of miss distance. The proposed robust guidance has the form of combination of the conventional PNG and the switching part. Several nonlinear engagement simulations show that the proposed guidance law is robust to the highly maneuvering target.
Keywords :
Lyapunov methods; missile guidance; proportional control; robust control; Lyapunov approach; PNG law; maneuvering target; miss distance estimation; missile guidance; nonlinear engagement simulations; robust proportional navigation guidance law; Acceleration; IP networks; Three-dimensional displays; Trajectory; Guidance Law; Miss distance; Robustness;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control, Automation and Systems (ICCAS), 2013 13th International Conference on
Conference_Location :
Gwangju
ISSN :
2093-7121
Print_ISBN :
978-89-93215-05-2
Type :
conf
DOI :
10.1109/ICCAS.2013.6703864
Filename :
6703864
Link To Document :
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