DocumentCode
2767589
Title
Modern guidance laws via receding horizon control without the time-to-go
Author
Kim, Ki Baek ; Kim, Myung-Joon ; Kwon, Wook Hyun
Author_Institution
Dept. of Electr. Eng., Seoul Nat. Univ., South Korea
Volume
4
fYear
1998
fDate
16-18 Dec 1998
Firstpage
4202
Abstract
A receding horizon guidance law (RHG) is proposed which is useful when the time-to-go is inaccurate or is unavailable, or the accurate time-to-go is difficult to estimate in a sampling time. In the presence of arbitrary target maneuvers and an initial lateral miss distance rate between the target and missile, it is shown that the proposed RHG can make lateral miss distance (MD) below the predescribed value in the prespecified time without the time-to-go. Through simulation, guidance performance of RHG is illustrated and RHG is compared with the optimal guidance law in terms of miss distance and missile acceleration
Keywords
missile guidance; optimal control; arbitrary target maneuvers; lateral miss distance; missile acceleration; modern guidance laws; optimal guidance law; receding horizon control; Acceleration; Cost function; Ear; Jamming; Missiles; Navigation; Optimal control; Pollution measurement; Radar; Sampling methods;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
Conference_Location
Tampa, FL
ISSN
0191-2216
Print_ISBN
0-7803-4394-8
Type
conf
DOI
10.1109/CDC.1998.761962
Filename
761962
Link To Document