| 挠性双自旋卫星的姿态稳定判据 |
| |
| 引用本文： | 金梁 Bauer,HF.挠性双自旋卫星的姿态稳定判据[J].宇航学报,1991(4):1-11. |
| |
| 作者姓名： | 金梁 Bauer HF |
| |
| 作者单位： | 国防科技大学，西德国防大学（Jnirersitdt der Bundeswehr Munchen） 湖南长沙，教授 |
| |
| 摘 要： | 本文建立了挠性双自旋卫星的姿态稳定性判据。挠性双自旋卫星由半刚性平台、转子以及固连于平台的挠性附件组成,选择由姿态角和模态坐标表示的系统的相对能量函数为Liapunov函数,由此建立的姿态稳定判据由两个部分组成,即忽略附件弹性运动时,半刚性双自旋卫星的姿态稳定条件和附件振动频率所应满足的条件。文中还给出了具体的应用例子。
|
| 关 键 词： | 卫星 双自旋 姿态 稳定 |
ATTITUDE STABILITY CRITERIA FOR DUAL SPINNING FLEXIBLE SATELLITES |
| |
| Jin Liang.ATTITUDE STABILITY CRITERIA FOR DUAL SPINNING FLEXIBLE SATELLITES[J].Journal of Astronautics,1991(4):1-11. |
| |
| Authors: | Jin Liang |
| |
| Abstract: | The attitude stability criteria for dual spinning flexible satellites is presented in this paper. The model of the dual spinning flexiblesatellite consists of a semi-rigid platform, rotor and a flexible appendege attached with a Panel, the relative energy function of the systemi s selected as a Liapunov function in terms of the attitude angles and mode coordinates, and the attitude stability criteria is obtained by using the Liapunov direct method. |
| |
| Keywords: | Flexible satellites Dual spinning Attitude stability Liapunov direct method |
| 本文献已被 CNKI 维普 等数据库收录！ |
