Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures

Title
Adaptive Integral-type Sliding Mode Control for Spacecraft Attitude Maneuvering Under Actuator Stuck Failures
Authors
Keywords
-
Journal
Chinese Journal of Aeronautics
Volume 24, Issue 1, Pages 32-45
Publisher
Elsevier BV
Online
2011-03-08
DOI
10.1016/s1000-9361(11)60005-8

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