Satellite Attitude Control with a Modified Iterative Learning Law for the Decrease in the Effectiveness of the Actuator

A fault tolerant satellite attitude control scheme with a modified iterative learning law is proposed for dealing with actuator faults. The actuator fault is modeled to reflect the degradation of actuation effectiveness, and the solar array-induced disturbance is considered as an external disturbanc...

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Bibliographic Details
Published inInternational journal of aeronautical and space sciences Vol. 11; no. 2; pp. 87 - 97
Main Authors Lee, Ho-Jin, Kim, You-Dan, Kim, Hee-Seob
Format Journal Article
LanguageKorean
Published 2010
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