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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Published in | International journal of aeronautical and space sciences Vol. 11; no. 2; pp. 87 - 97 |
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Main Authors | , , |
Format | Journal Article |
Language | Korean |
Published |
2010
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Subjects | |
Online Access | Get full text |
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