DocumentCode
3550552
Title
L2 stability and performance analysis of missile systems with linear autopilots and PN guidance laws
Author
Song, Seong-Ho ; Hong, Jin-Woo ; Ha, In-Joong
Author_Institution
Div. of Inf. Eng. & Telecommun., Hallym Univ., Gangwon, South Korea
fYear
2005
fDate
June 8-10, 2005
Firstpage
358
Lastpage
359
Keywords
Lyapunov methods; control system analysis; invariance; linear systems; missile guidance; stability; transfer functions; L2 stability; PN guidance laws; linear autopilots; linear time-invariant autopilot systems; missile systems; nonlinear planar pursuit; performance analysis; target acceleration; transfer function; Acceleration; Control systems; Equations; Missiles; Navigation; Performance analysis; Stability analysis; Sufficient conditions; Transfer functions; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2005. Proceedings of the 2005
ISSN
0743-1619
Print_ISBN
0-7803-9098-9
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2005.1469959
Filename
1469959
Link To Document