The hybrid attitude maneuver control of the three-axis stable liquid-filled spacecraft with large-deformation appendage-Reference-Cited by-同舟云学术

The hybrid attitude maneuver control of the three-axis stable liquid-filled spacecraft with large-deformation appendage

Published:2023-05-23 Issue: Volume: Page:
ISSN:2195-268X
Container-title:International Journal of Dynamics and Control
language:en
Short-container-title:Int. J. Dynam. Control

Author:

Shen Yunfeng,Shi Haoxiang,Fan Zhiwen,Song Xiaojuan^ORCID

Funder

National Natural Science Foundation of China

Innovative Research Group Project of the National Natural Science Foundation of China

Innovative Team and Outstanding Talent Program of Colleges and Universities in Guangxi

Central University Basic Research Fund of China

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Control and Optimization,Mechanical Engineering,Modeling and Simulation,Civil and Structural Engineering,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s40435-023-01204-7.pdf

Reference35 articles.

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2. Navabi M, Davoodi A, Reyhanolu M (2022) Optimum fuzzy sliding mode control of fuel sloshing in a spacecraft using PSO algorithm. Acta Astronaut 167:331–342

3. Navabi M, Davoodi A, Reyhanolu M (2019) Modeling and control of a nonlinear coupled spacecraft-fuel system. Acta Astronaut 162:436–446

4. Song XJ, Lu SF (2019) Attitude maneuver control of liquid-filled spacecraft with unknown inertia and disturbances. J Vib Control 25(8):1460–1469

5. Song XJ, Li XS, Lu SF et al (2022) Adaptive quaternion feedback control and oscillation suppression for liquid-filled flexible spacecraft. J Vib Eng Technol 7:1–18

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