DocumentCode :
391722
Title :
Fighter aircraft at high angles of attack
Author :
Calise, A.J. ; Johnson, M. ; Shin, Y.
Author_Institution :
Georgia Institute of Technology
Volume :
2
fYear :
2002
fDate :
4-7 Aug. 2002
Firstpage :
144
Lastpage :
147
Keywords :
Adaptive control; Aerodynamics; Aerospace control; Aircraft propulsion; Military aircraft; Output feedback; Programmable control; Shape control; Uncertainty; Vehicle dynamics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Circuits and Systems, 2002. MWSCAS-2002. The 2002 45th Midwest Symposium on
Print_ISBN :
0-7803-7523-8
Type :
conf
DOI :
10.1109/MWSCAS.2002.1186818
Filename :
1186818
Link To Document :
https://search.ricest.ac.ir/dl/search/defaultta.aspx?DTC=49&DC=391722
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