THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE

Bao Guang-wei; Liu Yan-zhu

doi:10.11728/cjss1993.01.031

Volume 13 Issue 1

Jan. 1993

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Article Navigation > Chinese Journal of Space Science > 1993 > 13(1): 31-38

Bao Guang-wei, Liu Yan-zhu. THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE[J]. Chinese Journal of Space Science, 1993, 13(1): 31-38. doi: 10.11728/cjss1993.01.031

Citation:

Bao Guang-wei, Liu Yan-zhu. THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE[J]. Chinese Journal of Space Science, 1993, 13(1): 31-38. doi: 10.11728/cjss1993.01.031

Bao Guang-wei, Liu Yan-zhu. THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE[J]. Chinese Journal of Space Science, 1993, 13(1): 31-38. doi: 10.11728/cjss1993.01.031

Citation:

Bao Guang-wei, Liu Yan-zhu. THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE[J]. Chinese Journal of Space Science, 1993, 13(1): 31-38. doi: 10.11728/cjss1993.01.031

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THE ALTITUDE STABILITY OF THREE-AXIS LIQUID FILLED SATELLITE

doi: 10.11728/cjss1993.01.031 cstr: 32142.14.cjss1993.01.031

Department of Engineering Mechanics, Shanghai Jiaotong University, 200030

Received Date: 1991-11-18
Rev Recd Date: 1900-01-01
Publish Date: 1993-01-24

Abstract

Abstract

This paper set up the equivalent mechanical model of the three-axis liquid filled satellite which has both translational and pitch-yaw disturbance. Then, using this model, the altitude stability of the satellite is investigated and a coincise analytic criterion is obtained.
- Liquid sloshing. Equivalent mechanical model,
- Altitude stability,