DocumentCode
425143
Title
Stability of modern guidance laws with model mismatch
Author
Weiss, Haim ; Hexner, Gyorgy
Author_Institution
RAFAEL, Haifa, Israel
Volume
4
fYear
2004
fDate
June 30 2004-July 2 2004
Firstpage
3634
Abstract
It is well known that modern guidance laws are capable of better performance than the traditional proportional navigation laws, provided that the missile model in the guidance law matches that of the actual missile. In this paper, we study the stability of modern guidance laws when the missile´s actual model differs from the model used in the design. The analysis is performed by means of Lyapunov functions and by means of the multivariable circle criterion.
Keywords
Lyapunov methods; control system analysis; control system synthesis; missile guidance; stability; Lyapunov functions; control system analysis; control system synthesis; missile model; modern guidance laws; multivariable circle criterion; proportional navigation laws; stability;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2004. Proceedings of the 2004
Conference_Location
Boston, MA, USA
ISSN
0743-1619
Print_ISBN
0-7803-8335-4
Type
conf
Filename
1384476
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