| 引用本文: | 凌德海.双自旋卫星的姿态稳定性判据.[J].国防科技大学学报,1982,(2):55-63.[点击复制] |
| Ling Dehai.Atitude Stability Criteria for Dual Spin Satellite[J].Journal of National University of Defense Technology,1982,(2):55-63[点击复制] |
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| 双自旋卫星的姿态稳定性判据 |
| 凌德海 |
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| 摘要: |
| 本文推证了一个双自旋卫星的姿态稳定性新判据。判据的论证基于没有活动部件但有能量耗散的半刚体概念，并且采用了有关系统稳定性的李雅普诺夫方法。然后，将这个结论同 Ioril1o、Landon，Likins 采用离散参数法和能沉法所得到的结论进行了比较[1]-[4]。 |
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| 投稿日期：1982-02-15 |
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| Atitude Stability Criteria for Dual Spin Satellite |
| Ling Dehai |
| Abstract: |
| A New Attitude stability criteria for Dual spin Satellite is developed in this paper.
The argument of this Criteria is based on a concept of Semirigid which has no moving parts but dissipates energy and also by means of Lyapunov method about system stability. Then this conclnsion is compared with conclnsions from a discrebe parameter approach and an energy sink approach developed by Iorillo，Landon and Likins[l]-[4]. |
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