Attitude Stability of a Spacecraft with Slosh Mass Subject to Parametric Excitation
The attitude motion of a spin-stabilized, upper-stage spacecraft is investigated based on a two-body model, consisting of a symmetric body, representing the spacecraft, and a spherical pendulum, representing the liquid slag pool entrapped in the aft section of the rocket motor. Exact time-varying no...
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| Format: | Article |
| Language: | English |
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Korean Space Science Society (KSSS)
2003-09-01
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| Series: | Journal of Astronomy and Space Sciences |
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| Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2003/v20n3/OJOOBS_2003_v20n3_205.pdf |