DocumentCode
1694724
Title
Wing Missiles Stabilization Based on Sliding Mode Control
Author
Shtessel, Yuri B.
Author_Institution
Department of Electrical & Computer Engineering, University of South Carolina
fYear
1993
Firstpage
574
Lastpage
578
Keywords
Accelerometers; Cities and towns; Control systems; Differential algebraic equations; Differential equations; Gyroscopes; Mathematics; Missiles; Sliding mode control; Switches;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
Type
conf
DOI
10.1109/AEROCS.1993.720999
Filename
720999
Link To Document