Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

Adaptive Nonsingular Terminal Sliding Mode Control for Attitude Tracking of Spacecraft With Actuator Faults

In this paper, an adaptive nonsingular terminal sliding mode control (ANTSMC) is investigated for attitude tracking of spacecraft with actuator faults. First, a nonsingular fast terminal sliding mode surface is designed to avoid the singularity. Finite-time attitude control is developed using the no...

Täydet tiedot

Bibliografiset tiedot
Päätekijät: Chenghu Jing, Hongguang Xu, Xinjian Niu, Xiaoming Song
Aineistotyyppi: Artikkeli
Kieli:English
Julkaistu: IEEE 2019-01-01
Sarja:IEEE Access
Aiheet:
Spacecraft
nonsingular terminal sliding mode
adaptive
finite time
attitude control
actuator faults
Linkit:https://ieeexplore.ieee.org/document/8657691/

Internet

https://ieeexplore.ieee.org/document/8657691/

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