DocumentCode :
315901
Title :
Refining the Shuttle training aircraft controller
Author :
Berenji, Hamid R. ; Chang, Ping-Wei ; Swanson, Steven R.
Author_Institution :
Div. of Comput. Sci., NASA Ames Res. Center, Moffett Field, CA, USA
Volume :
2
fYear :
1997
fDate :
1-5 Jul 1997
Firstpage :
677
Abstract :
NASA uses the Shuttle training aircraft (STA) to train the Shuttle pilot astronauts. Although as compared to the Shuttle, STA is a small aircraft, it does simulate, with some model following errors, the aerodynamics of the Shuttle. In this paper, we show how these differences can be reduced significantly by using a new pitch predict controller and a new adaptive fuzzy controller. In particular, we show how the collaborative work between NASA Ames and the Shuttle Training Branch of Johnson Space Center has improved the accuracy of STA model following from its current level of 71% to 91% which is equivalent to a 69% error reduction
Keywords :
adaptive control; aerospace simulation; aircraft control; fuzzy control; identification; predictive control; training; two-term control; NASA; PD control; adaptive control; aerodynamics; fuzzy control; identification; model following errors; pitch predict controller; shuttle training aircraft; training; Aerospace control; Aircraft; Control systems; Fuzzy control; NASA; PD control; Proportional control; Servomechanisms; Space shuttles; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Fuzzy Systems, 1997., Proceedings of the Sixth IEEE International Conference on
Conference_Location :
Barcelona
Print_ISBN :
0-7803-3796-4
Type :
conf
DOI :
10.1109/FUZZY.1997.622793
Filename :
622793
Link To Document :
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