DocumentCode
2769256
Title
Advanced missile guidance with hybrid system models
Author
Cong, Shan ; Hong, Lang ; Chen, Genshe
Author_Institution
Dept. of Electr. Eng., Wright State Univ., Dayton, OH, USA
Volume
4
fYear
1998
fDate
16-18 Dec 1998
Firstpage
4714
Abstract
In this paper, two multiple model guidance laws are proposed: one is called the mixture model guidance, the other is called the cooperative multiple model guidance. Both approaches are suboptimal guidance laws for intercept problems with hybrid system models, and can cooperate with multiple model filtering algorithms, such as the interacting multiple model filter
Keywords
filtering theory; missile guidance; probability; state estimation; suboptimal control; cooperative multiple model guidance; filtering algorithms; hybrid system models; interception; missile guidance; mixture model guidance; probability; state estimation; suboptimal control; Filtering algorithms; Filters; Missiles; Optimal control; Power system modeling; Predictive models; Riccati equations; State estimation; Statistics; Uncertainty;
fLanguage
English
Publisher
ieee
Conference_Titel
Decision and Control, 1998. Proceedings of the 37th IEEE Conference on
Conference_Location
Tampa, FL
ISSN
0191-2216
Print_ISBN
0-7803-4394-8
Type
conf
DOI
10.1109/CDC.1998.762078
Filename
762078
Link To Document