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- W56640462 abstract "ABSTRACT In this paper, reorientation based on angular momentum exchange is applied for a bias momentum stabilized satellite, which is equipped with a spheric al fuel tank, and the effect of liquid slosh on the attitude properties such as inertia tensor and angular rate is investigated. In order to represent the slosh motion of liquid an equivalent mechanical model is adopted and full nonlinear equations of motion for three-body system are derived. Computer simulations are performed for several cases, which use the viscosity of liquid and the center location of the tank as input parameters, mainly in order to observe how the viscosity of liquid and the center location of the tank influen ce the spacecraft’s attitude. The investigation includes observing time-variations of the inertia tensor, especially presence of components of product of inertia during the maneuver.key Words : Attitude Acquisition(자세 획득), Inertia Tensor(관성 텐서), Liquid Slosh(액체 유동), Reorientation(방향전환) 2009년 2월 27일 접수 ~2009년 3월 26일 심사완료* 한국항공대학교 항공운항학과** 한국항공대학교 항공우주 및 기계공학부 연락저자, E-mail : slee@kau.ac.kr 경기도 고양시 덕양구 화전동 200-1" @default.
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- W56640462 date "2009-01-01" @default.
- W56640462 modified "2023-09-23" @default.
- W56640462 title "Effects of Liquid Fuel on Spacecraft's Moment of Inertia and Motion during Reorientation" @default.
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