Two‐Layer Terminal Sliding Mode Attitude Control of Satellites Equipped with Reaction Wheels-Reference-Cited by-同舟云学术

Two‐Layer Terminal Sliding Mode Attitude Control of Satellites Equipped with Reaction Wheels

Published:2018-07-30 Issue:1 Volume:22 Page:388-397
ISSN:1561-8625
Container-title:Asian Journal of Control
language:en
Short-container-title:Asian Journal of Control

Author:

Bayat Farhad¹^ORCID,Javaheri Mojtaba¹

Affiliation:

1. Department of Electrical EngineeringUniversity of Zanjan Zanjan Iran

Publisher

Wiley

Subject

Control and Systems Engineering

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/asjc.1878

Reference33 articles.

1. Spacecraft Attitude Determination and Control

2. Nonlinear Analysis and Attitude Control of a Gyrostat Satellite with Chaotic Dynamics Using Discrete-Time LQR-OGY

3. Attitude guidance and tracking for spacecraft with two reaction wheels

4. Bolandi H. F.Bayat andM.Nasirian “Attitude control of spinning satellite subject to actuators restriction using eigenstructure assignment ”1st Int. Symp. Syst. Control Aerosp. Astronaut. Harbin China pp.7–14(2006).

5. Sliding-mode adaptive attitude controller design for spacecrafts with thrusters

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