Satellite attitude PDE-based controller design considering fluid fuel sloshing in planar maneuver-Reference-Cited by-同舟云学术

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Satellite attitude PDE-based controller design considering fluid fuel sloshing in planar maneuver

Published:2022-03 Issue: Volume:122 Page:107366
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Jokar Meysam^ORCID,Salarieh Hassan,Nejat Pishkenari Hossein^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference65 articles.

1. Multibody dynamics and robust attitude control of a MW-level solar power satellite;Zhang;Aerosp. Sci. Technol.,2021

2. Hybrid control of a satellite with membrane antenna considering nonlinear vibration;Liu;Aerosp. Sci. Technol.,2021

3. Boundary control of anti-symmetric vibration of satellite with flexible appendages in planar motion with exponential stability;Rad;Acta Astronaut.,2018

4. Boundary control design based on partial differential equation observer for vibration suppression and attitude control of flexible satellites with multi-section solar panels;Ataei;J. Vib. Control,2021

5. Vibration control for a flexible satellite system with output constraints;Meng;Nonlinear Dyn.,2016

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