Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity

Yuji Tanaka, Mitsuhisa Baba, Masatsugu Otsuki, Kazuhisa Fujita, Takehiro Himeno, Takao Maeda, Masaki Takahashi. Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity. In 61st IEEE Conference on Decision and Control, CDC 2022, Cancun, Mexico, December 6-9, 2022. pages 3092-3097, IEEE, 2022. [doi]

Abstract

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