Large Motion Dynamics of In-Orbit Flexible Spacecraft with Large-Amplitude Propellant Slosh-Reference-Cited by-同舟云学术

Large Motion Dynamics of In-Orbit Flexible Spacecraft with Large-Amplitude Propellant Slosh

Author:

Feng Liu¹,Baozeng Yue¹,Banerjee Arun K.¹,Yong Tang²,Wenjun Wu³,Zhengyong Liu⁴

Affiliation:

1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China

2. Guangdong Institute of Aeronautics and Astronautics Equipment & Technology, 519000 Zhuhai, Guangdong, People’s Republic of China

3. Guangxi University of Science and Technology, 545006 Liuzhou, Guangxi, People’s Republic of China

4. Shanghai Aerospace Systems Engineering Institute, 201109 Shanghai, People’s Republic of China

Funder

Guangxi Natural Science Foundation

National Natural Science Foundation of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference24 articles.

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