DocumentCode :
2866214
Title :
An adaptive flight control system based on an explicit parameter identification technique
Author :
Smith, Ronald ; Speyer, Jason L.
Author_Institution :
The University of Texas at Austin
fYear :
1989
fDate :
1989
Firstpage :
483
Lastpage :
487
Keywords :
Acceleration; Accelerometers; Adaptive control; Adaptive systems; Aerospace control; Aircraft; Equations; Parameter estimation; Programmable control; Stability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control and Applications, 1989. Proceedings. ICCON '89. IEEE International Conference on
Type :
conf
DOI :
10.1109/ICCON.1989.770564
Filename :
770564
Link To Document :
بازگشت