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Keywords: additive actuator fault
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Journal Articles
Publisher: ASME
Article Type: Research Papers
J. Dyn. Sys., Meas., Control. September 2011, 133(5): 051006.
Published Online: August 1, 2011
... = 1 , 2 , 3 ɛ i and λ and γ are positive constants with λ > 1. T heorem 2. Consider the rigid spacecraft attitude control problem with additive actuator faults and the partial loss of actuator effectiveness defined by Eqs. 3 , 4 , 5 . The control law defined in Eq. 28...