DocumentCode
1032
Title
Development of 3-D Modified Proportional Navigation Guidance Law against High-Speed Targets
Author
Yu-Ping Lin ; Chun-Liang Lin ; Yun-Hao Li
Author_Institution
Dept. of Electr. Eng., Nat. Chung Hsing Univ., Taichung, Taiwan
Volume
49
Issue
1
fYear
2013
fDate
Jan. 2013
Firstpage
677
Lastpage
687
Abstract
The work presented here proposes a terminal guidance law against very high-speed targets. Proportional navigation guidance (PNG) is mostly effective for interceptors and targets with ideal dynamics and constant speeds during the collision course, however, it is nonrobust for the objects with nonconstant speeds, such as the interceptor equipped with thrust-vector-control (TVC). To resolve the problem the interceptor considered here is guided by a 3-dimensional (3-D) modified proportional navigation guidance (MPNG) law, which is developed to account for the interceptor´s axial acceleration. The guidance law is potentially applicable to interceptors with TVC to provide lateral accelerations.
Keywords
missile control; missile guidance; 3D modified proportional navigation guidance law; MPNG; TVC; collision course; high-speed targets; interceptor axial acceleration; lateral accelerations; thrust vector control; Acceleration; Estimation; Missiles; Navigation; Neural networks; Trajectory; Vectors;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.2013.6404133
Filename
6404133
Link To Document