Modeling and Control of Fuel Sloshing and its Effect on Spacecraft Attitude
Sloshing phenomenon in spacecraft fuel tank during orbital maneuver, causes adverse effects on spacecraft attitude. Therefore, before orbital maneuvers, modeling fuel sloshing and determining appropriate method for controlling it has to be carried out. The aim of this paper is to model slosh dynamic...
| Main Authors: | , |
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| Format: | Article |
| Language: | fas |
| Published: |
Aerospace Research Institute
2019-02-01
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| Series: | فصلنامه علوم و فناوری فضایی |
| Subjects: | |
| Online Access: | https://jsst.ias.ir/article_81881_b54b34591d4b6caa29d1edfd2fbb0751.pdf |