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 :
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