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