Improved Moving Pulsating Ball Equivalent Model for Large-Amplitude Liquid Slosh
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061622
Reference20 articles.
1. Liquid Sloshing Dynamics
2. Hybrid Control of Liquid-Filled Spacecraft Maneuvers by Dynamic Inversion and Input Shaping
3. Influence of liquid sloshing on dynamics of flexible space structures
4. Influence of the ATV Propellant Sloshing on the GNC Performance
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