| Accession number;00A0150769 |
| Title;Planning of Thruster Activation for Orbit Maintenance Vehicle. |
| Author;TODA YOSHITSUGU(Electrotech. Lab., Agency of Ind. Sci. and Technol.) IWATA TOSHIAKI(Electrotech. Lab., Agency of Ind. Sci. and Technol.) MACHIDA KAZUO(Electrotech. Lab., Agency of Ind. Sci. and Technol.) SATO HITOSHI(Shimizu Corp.) AOKI SHIGERU(Shimizu Corp.) YOSHIDA TETSUJI(Shimizu Corp.) |
Journal Title;Proceedings of the Space Sciences and Technology Conference
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Journal Code:S0277A
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ISSN:
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VOL.43rd;NO.;PAGE.83-87(1999)
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| Figure&Table&Reference;FIG.4 |
| Pub. Country;Japan |
| Language;Japanese |
| Abstract;As spacecrafts are in the 3 dimensional space, they can fly with 6 active actuaters. Any spacecraft has the redundant thruster system. In this paper, the thruster selection rule algorithm is presented. (author abst.) |
