DocumentCode :
2867418
Title :
Control law design and test of an experimental flutter margin augmentation system for an airplane
Author :
Koenig, Klaus ; Luckner, Robert
Author_Institution :
MBB-UT
fYear :
1989
fDate :
1989
Firstpage :
806
Lastpage :
811
Keywords :
Aerospace control; Aircraft; Airplanes; Blades; Control systems; Open loop systems; Optimal control; Sensor phenomena and characterization; System testing; Transfer functions;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Applications, 1989. Proceedings. ICCON '89. IEEE International Conference on
Type :
conf
DOI :
10.1109/ICCON.1989.770633
Filename :
770633
Link To Document :
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