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 :
بازگشت