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 :
https://search.ricest.ac.ir/dl/search/defaultta.aspx?DTC=49&DC=3550552
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