Integrated Adaptive Control for Spacecraft Attitude and Orbit Tracking Using Disturbance Observer-Reference-Cited by-同舟云学术

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Integrated Adaptive Control for Spacecraft Attitude and Orbit Tracking Using Disturbance Observer

Published:2021-02-26 Issue:4 Volume:22 Page:936-947
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Xia Kewei,Eun Youngho,Lee Taeyang,Park Sang-Young^ORCID

Funder

National Research Foundation of Korea funded by the Ministry of Science and ICT

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-021-00359-x.pdf

Reference31 articles.

1. Kristiansen R, Nicklasson PJ, Gravdahl JT (2008) Spacecraft coordination control in 6DOF: integrator backstepping vs passivity-based control. Automatica 44(11):2896–2901

2. Kristiansen R, Nicklasson PJ (2009) Spacecraft formation flying: a review and new results on state feedback control. Acta Astronaut 65(11):1537–1552

3. Bae J, Kim Y (2012) Adaptive controller design for spacecraft formation flying using sliding mode controller and neural networks. J Frankl Inst 349(2):578–603

4. Huang P, Zhang F, Cai J, Wang D, Meng Z, Guo J (2017) Dexterous tethered space robot: design, measurement, control, and experiment. IEEE Trans Aerosp Electron Syst 53(3):1452–1468

5. Zhang F, Huang P (2017) Releasing dynamics and stability control of maneuverable tethered space net. IEEE/ASME Trans Mechatron 22(2):983–993

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1. Experimental and Numerical Investigation on Attitude Adjustment Characteristics of Spacecraft with Impulse Thruster;International Journal of Aeronautical and Space Sciences;2024-09-09

2. Novel scheme for uncertainty and disturbance estimation to control of spacecraft system with input constraint;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2024-07-31

3. Strong Robust Attitude Control of the Large Launch Vehicle Based on Backstepping Design Approach;2024 36th Chinese Control and Decision Conference (CCDC);2024-05-25

4. Underactuated Attitude–Orbit Coupling Control for Microsatellite Based on a Single Orbital Thruster;IEEE Transactions on Aerospace and Electronic Systems;2024-04

5. Fixed-time fuzzy disturbance observer–based adaptive integral sliding-mode spacecraft attitude control under time-varying output constraints;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2024-01-16

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