Finite-Time Attitude Consensus Tracking Control of Multiple Spacecraft Systems With Input Quantization and Actuator Faults

This paper investigates the finite-time attitude consensus tracking problem for multiple spacecraft systems in the presence of input quantization, external disturbances and actuator faults. First, the input quantization is decomposed into a combination of a linear term and a disturbance-like term. T...

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Bibliographic Details

Published in:	IEEE Access
Main Authors:	Dandan Zhang, Weiyu Liu, Heng Zhang
Format:	Article
Language:	English
Published:	IEEE 2024-01-01
Subjects:	Multiple spacecraft systems finite-time attitude consensus tracking input quantization actuator faults adding a power integrator
Online Access:	https://ieeexplore.ieee.org/document/10695065/