Spacecraft nutation inhibition method for low-orbit geomagnetic energy storage in-orbit delivery
文献类型：专利
| 作者 | Li WH(李文皓) ; Zhang H(张珩); Feng GH(冯冠华); Chen Zhang; Lei Yang; Linli Lv; Zhang H(张珩); Li WH(李文皓); Feng GH(冯冠华)
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| 发表日期 | 2022-12-20 |
| 专利号 | US11530054B2 |
| 著作权人 | INSTITUTE OF MECHANICS, CHINESE ACADEMY OF SCIENCES ; GUANGDONG ACADEMY OF AEROSPACE RESEARCH IMECH, CAS |
| 国家 | 美国 |
| 英文摘要 | A spacecraft nutation inhibition method for low-orbit geomagnetic energy storage in-orbit delivery includes: S1, enabling a delivery connection rod to be slidably connected to two mass blocks in a length direction, and adjusting the center of mass of a spacecraft system to pass through a main connecting shaft; S2, respectively measuring, calibrating and adjusting the center of mass and the principal axis of inertia of the delivery connection rod that is to deliver the space target or de-orbit debris; S3, carrying out energy storage delivery; S4, respectively adjusting the center of mass and the moment of inertia of the delivery connection rod after delivering the space target or de-orbit debris; S5, carrying out energy dissipation and unloading; and S6, enabling the spacecraft system to prepare to grab the next space target or de-orbit debris and proceeding to the next delivery work cycle. |
| 分类号 | 发明授权 |
| 申请日期 | 2020-06-23 |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/99967]  |
| 专题 | 宽域飞行工程科学与应用中心 |
| 推荐引用方式 GB/T 7714 | Li WH,Zhang H,Feng GH,et al. Spacecraft nutation inhibition method for low-orbit geomagnetic energy storage in-orbit delivery. US11530054B2. 2022-12-20. |
入库方式： OAI收割
来源：力学研究所
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