Yuji Tanaka et al.: Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity. (2022)conf/cdc/TanakaBOFHMT2210.1109/CDC51059.2022.9992643Space Lander Descent Control System Design Considering Fuel Sloshing Under Microgravity.7Yuji Tanaka1Mitsuhisa Baba2Masatsugu Otsuki3Kazuhisa Fujita4Takehiro Himeno5Takao Maeda6Masaki Takahashi73092-3097CDCCDC20222022provenance information for RDF data of dblp record 'conf/cdc/TanakaBOFHMT22'2023-09-30T09:36:22+0200