Neural-Network Based Finite-Time Coordinated Formation Control for Spacecraft Without Unwinding

This paper investigates the problem of rotation matrix-based attitude synchronization and tracking control for spacecraft formation flying exposed to external disturbance and unknown inertial matrix. For the purpose of ensuring finite-time convergence for attitude tracking errors, a hyperbolic tange...

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Bibliographic Details
Main Authors: Yong Hao, Yushan He, Yaen Xie, Cong Sun, Kun Zhao
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Online Access:https://ieeexplore.ieee.org/document/9133531/