CN107600463B - 一种敏捷小卫星姿态快速机动控制方法 - Google Patents
一种敏捷小卫星姿态快速机动控制方法 Download PDFInfo
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CN109131942B (zh) * | 2018-10-29 | 2020-03-17 | 上海微小卫星工程中心 | 一种用于对卫星的旋转体进行消旋控制的方法及相应消旋装置 |
CN111460634B (zh) * | 2020-03-18 | 2023-05-23 | 长光卫星技术股份有限公司 | 一种微小微星磁力矩器多目标设计方法 |
CN112046795B (zh) * | 2020-08-31 | 2022-04-15 | 长光卫星技术股份有限公司 | 一种基于轨控偏差力矩系数标定的小卫星轨控优化方法 |
CN114115305B (zh) * | 2021-11-01 | 2022-10-04 | 武汉大学 | 一种姿态快速机动的高精度遥感小卫星的控制***设计方法 |
CN113968362B (zh) * | 2021-11-16 | 2023-07-07 | 长光卫星技术股份有限公司 | 一种卫星在轨自主三轴快速机动控制方法 |
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CN101219714A (zh) * | 2007-12-26 | 2008-07-16 | 北京航空航天大学 | 双框架磁悬浮控制力矩陀螺 |
CN104483972A (zh) * | 2014-10-31 | 2015-04-01 | 上海新跃仪表厂 | 一种航天器流体环反作用执行机构 |
CN105644810A (zh) * | 2016-02-05 | 2016-06-08 | 上海微小卫星工程中心 | 一种开环控制反作用轮转速变化及卸载方法 |
CN106828980A (zh) * | 2016-11-21 | 2017-06-13 | 上海卫星工程研究所 | 星上有效载荷扫描机构大干扰力矩实时补偿方法 |
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WO2006004581A2 (en) * | 2004-04-06 | 2006-01-12 | University Of North Texas | Clutch driven reaction wheel steering unit |
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CN101219714A (zh) * | 2007-12-26 | 2008-07-16 | 北京航空航天大学 | 双框架磁悬浮控制力矩陀螺 |
CN104483972A (zh) * | 2014-10-31 | 2015-04-01 | 上海新跃仪表厂 | 一种航天器流体环反作用执行机构 |
CN105644810A (zh) * | 2016-02-05 | 2016-06-08 | 上海微小卫星工程中心 | 一种开环控制反作用轮转速变化及卸载方法 |
CN106828980A (zh) * | 2016-11-21 | 2017-06-13 | 上海卫星工程研究所 | 星上有效载荷扫描机构大干扰力矩实时补偿方法 |
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Address after: No. 1299, Mingxi Road, Beihu science and Technology Development Zone, Changchun City, Jilin Province Patentee after: Changguang Satellite Technology Co.,Ltd. Address before: No.1759 Mingxi Road, Gaoxin North District, Changchun City, Jilin Province Patentee before: CHANG GUANG SATELLITE TECHNOLOGY Co.,Ltd. |
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Denomination of invention: A Fast Maneuver Control Method for Agile Small Satellite Attitude Granted publication date: 20190524 Pledgee: Jilin credit financing guarantee Investment Group Co.,Ltd. Pledgor: Changguang Satellite Technology Co.,Ltd. Registration number: Y2024220000032 |