Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity-Reference-Cited by-同舟云学术

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Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity

Published:2022-12-06 Issue: Volume: Page:
ISSN:
Container-title:2022 IEEE 61st Conference on Decision and Control (CDC)
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Author:

Tanaka Yuji¹,Baba Mitsuhisa²,Otsuki Masatsugu²,Fujita Kazuhisa²,Himeno Takehiro³,Maeda Takao⁴,Takahashi Masaki⁵

Affiliation:

1. Keio University,School of Science for Open and Environmental Sytems,Kanagawa,Japan

2. Japan Aerospace Exploration Agency,Kanagawa,Japan,252-5210

3. University of Tokyo,Department of Aeronautics and Astronautics,Tokyo,Japan,113-8656

4. Tokyo University of Agriculture and Technology,Department of Mechanical Systems Engineering,Tokyo,Japan,184-8588

5. Keio Univerisity,Department of System Design Engineering,Kanagawa,Japan

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/9992315/9992317/09992643.pdf?arnumber=9992643

Reference26 articles.

1. The Dynamic Behavior of Liquids in Moving Containers;Abramson;NASA SP-106,1967

2. Dynamics of Low-Gravity Sloshing in Spherical Tanks during Touchdown Phases of Landers

3. Microgravity experiments of sampling and landing technologies for Martian Moons eXploration (MMX) in ZARM Drop Tower;Baba

4. Liquid Sloshing Dynamics

5. The New Dynamic Behavior of Liquids in Moving Containers;Dodge,2000

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