DocumentCode
1246300
Title
A modified CLOS guidance law via right inversion
Author
Jie Huang ; Ching-Fang Lin
Author_Institution
American GNC Corp., Canoga Park, CA, USA
Volume
31
Issue
1
fYear
1995
Firstpage
491
Lastpage
495
Abstract
A command to line-of-sight (CLOS) guidance law is derived via right inversion. This CLOS guidance law achieves the same objective as that given by Ha and Chong via feedback linearization (1992) yet is considerably simpler. This is made possible by reformulating the original nonlinear tracking problem as a right inversion problem for a linear time-varying system, and by making use of the orthogonal property of a rotational matrix.<>
Keywords
digital simulation; feedback; linearisation techniques; matrix algebra; missile guidance; time-varying systems; command to line-of-sight; feedback linearization; linear time-varying system; modified CLOS guidance; nonlinear tracking; orthogonal property; right inversion; right inversion problem; rotational matrix; Acceleration; Feedback; Filters; Missiles; Parity check codes; Redundancy; Robustness; Time varying systems; Uncertain systems; Uncertainty;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.366334
Filename
366334
Link To Document