Constrained Nonsingular Terminal Sliding Mode Attitude Control for Spacecraft: A Funnel Control Approach

Constrained Nonsingular Terminal Sliding Mode Attitude Control for Spacecraft: A Funnel Control Approach

This paper presents an adaptive constrained attitude control for uncertain spacecraft. Inspired by the concept of nonsingular terminal sliding mode control and funnel control for nonlinear systems, a novel adaptive attitude control is introduced which contains a time-varying gain to handle the const...

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Bibliographic Details
Main Authors: Nguyen Xuan-Mung, Mehdi Golestani, Sung Kyung Hong
Format: Article
Language:English
Published: MDPI AG 2023-01-01
Series:Mathematics
Subjects:
spacecraft attitude control
sliding mode control
constrained control
fixed-time stability
Online Access:https://www.mdpi.com/2227-7390/11/1/247

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