Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking

Predefined Time Anti-Unwinding Control of Rigid Spacecraft Attitude Tracking

This paper addresses the predefined time anti-unwinding attitude tracking control of rigid spacecraft with inertial uncertainties and external disturbances. Firstly, a new predefined-time terminal sliding surface (FTS) is proposed with hybrid technique. Secondly, a simple predefined-time sliding mod...

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Bibliographic Details
Main Authors: Liangmou Hu, Zeng Wang, Hanghang Wang, Changrui Chen, Heng Yue, Jiale Wang
Format: Article
Language:English
Published: IEEE 2025-01-01
Series:IEEE Access
Subjects:
Attitude tracking control
predefined-time
unwinding problem
uncertain spacecraft
robustness
Online Access:https://ieeexplore.ieee.org/document/10839419/
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https://ieeexplore.ieee.org/document/10839419/

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