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