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• W2023894954 startingPage "368" @default.
• W2023894954 abstract "In this paper, an adaptive fast terminal sliding mode control control law (AFTSMCL) is presented to resolve attitude tracking control problem for rigid spacecraft, which can provide finite-time convergence, strong robustness, and fault-tolerant control. Rigorous proof is achieved first. Simulation results are presented to illustrate the effectiveness of presented control law." @default.
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• W2023894954 date "2016-01-01" @default.
• W2023894954 modified "2023-09-29" @default.
• W2023894954 title "Finite-Time Tracking Control of Rigid Spacecraft Under Actuator Saturations and Faults" @default.
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• W2023894954 doi "https://doi.org/10.1109/tase.2014.2379615" @default.
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