Tan-Type BLF-Based Attitude Tracking Control Design for Rigid Spacecraft with Arbitrary Disturbances

Tan-Type BLF-Based Attitude Tracking Control Design for Rigid Spacecraft with Arbitrary Disturbances

This study deals with the problem of disturbances in observer-based attitude tracking control for spacecraft in the presence of inertia-matrix uncertainty and arbitrary disturbance. Following the backstepping control, a tan-type barrier Lyapunov function (BLF)-based attitude tracking control method...

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Bibliographic Details
Main Authors: Nguyen Xuan-Mung, Mehdi Golestani, Sung-Kyung Hong
Format: Article
Language:English
Published: MDPI AG 2022-12-01
Series:Mathematics
Subjects:
spacecraft attitude system
tan-type BLF
prescribed time stability
backstepping control
Online Access:https://www.mdpi.com/2227-7390/10/23/4548

Internet

https://www.mdpi.com/2227-7390/10/23/4548

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