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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Bibliografski detalji

Glavni autori:	Liangmou Hu, Zeng Wang, Hanghang Wang, Changrui Chen, Heng Yue, Jiale Wang
Format:	Artigo
Jezik:	Inglês
Izdano:	IEEE 2025-01-01
Serija:	IEEE Access
Teme:	Attitude tracking control predefined-time unwinding problem uncertain spacecraft robustness
Online pristup:	https://ieeexplore.ieee.org/document/10839419/
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