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International Journal of Aerospace Engineering
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2021
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Article
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Tab 2
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Review Article
Adaptive Fixed-Time Nonsingular Terminal Sliding Mode Attitude Tracking Control for Spacecraft with Actuator Saturations and Faults
Table 2
The results on comparison of different controllers.
FNTSM control law performance
(17) in this paper
(25) in [
24
]
Quaternion error
Angular velocity error
FNTSM/NFTSM error
Convergence time(s)
9.97
11.01