Hyperbolic Tangent Function-Based Finite-Time Sliding Mode Control for Spacecraft Rendezvous Maneuver Without Chattering

Hyperbolic Tangent Function-Based Finite-Time Sliding Mode Control for Spacecraft Rendezvous Maneuver Without Chattering

This paper investigates the robust finite-time rendezvous maneuver control for spacecraft via sliding mode control technology. Two control architectures are devised for realizing the control objective, where a novel-developed sliding mode surface (SMS) is designed by resorting to the hyperbolic tang...

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Bibliographic Details
Main Authors: Zhen Shi, Chengchen Deng, Sai Zhang, Yaen Xie, Hongtao Cui, Yong Hao
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Spacecraft rendezvous maneuver
finite-time control
sliding mode control
chattering problem
adaptive control
Online Access:https://ieeexplore.ieee.org/document/9052448/

Internet

https://ieeexplore.ieee.org/document/9052448/

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