Adaptive Integral-Sliding-Mode Control for Spacecraft Single-Axis Pointing Using Two Torques

Adaptive Integral-Sliding-Mode Control for Spacecraft Single-Axis Pointing Using Two Torques

This paper deals with the attitude control problem of a nearly axis-symmetric spacecraft actuated by two torques perpendicular to its symmetry axis. As a result, the spacecraft symmetry axis is unactuated and the rotation about it is uncontrollable. Our objective aims to stabilize the symmetry axis...

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Bibliographic Details
Main Authors: Tao Wang, Yingchun Zhang
Format: Article
Language:English
Published: IEEE 2020-01-01
Series:IEEE Access
Subjects:
Adaptation
fault tolerance
finite-time
integral sliding modes
axis-symmetric spacecraft
spin-axis stabilization
Online Access:https://ieeexplore.ieee.org/document/9296746/

Internet

https://ieeexplore.ieee.org/document/9296746/

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