DocumentCode
1421355
Title
Three-Dimension
Guidance Law and Capture Region Analysis
Author
Liu, Li-jun ; Shen, Yi
Author_Institution
Harbin Inst. of Technol., Harbin, China
Volume
48
Issue
1
fYear
2012
Firstpage
419
Lastpage
429
Abstract
A new three-dimension nonlinear H∞ guidance law is proposed to intercept an unknown maneuvering target. By using the modified polar coordinate (MPC), nonlinear relative motion equations only contain three state variables. Then we apply the nonlinear H∞ control theory into system equations to get an analytic H∞ guidance law, which has the same expression as true proportional navigation (TPN). The proposed H∞ guidance law can ensure system L2 gain less than or equal to a positive constant. Some results of performance analysis including capture region, capture region with acceleration constraint, an integral expression of time-to-go, and miss distance are derived analytically. Particularly, the capture region with acceleration constraint is an important improvement upon the capture region of TPN and is significant for applications. Finally, some numerical examples illustrate the theories clearly, and some simulations are conducted to validate the academic results.
Keywords
H∞ control; acceleration control; missile control; motion control; nonlinear control systems; acceleration constraint; capture region analysis; maneuvering target; missile body; modified polar coordinate; nonlinear H∞ control theory; nonlinear relative motion equation; system equation; three-dimension nonlinear H∞ guidance law; true proportional navigation; Acceleration control; Equations; Mathematical model; Missiles; Navigation; Vectors;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/TAES.2012.6129645
Filename
6129645
Link To Document