Design of Flight Control System Based on Adaptive Backstepping Method for a Space Transportation System

This paper presents a new guidance and control system based on an adaptive backstepping method for a space transportation system. In recent years, many studies of flight control systems using feedback linearization combined with time-scale separation have been carried out. Since this type of control...

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Veröffentlicht in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2015, Vol.58(2), pp.55-65
Hauptverfasser: ABE, Akio, IWAMOTO, Kohei, SHIMADA, Yuzo
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Sprache:eng
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