CN112278329B - 一种用于遥感卫星定姿的非线性滤波方法 - Google Patents
一种用于遥感卫星定姿的非线性滤波方法 Download PDFInfo
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- CN112278329B CN112278329B CN202011188696.7A CN202011188696A CN112278329B CN 112278329 B CN112278329 B CN 112278329B CN 202011188696 A CN202011188696 A CN 202011188696A CN 112278329 B CN112278329 B CN 112278329B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/244—Spacecraft control systems
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/244—Spacecraft control systems
- B64G1/245—Attitude control algorithms for spacecraft attitude control
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CN113815903B (zh) * | 2021-09-06 | 2023-06-23 | 长光卫星技术股份有限公司 | 一种用于遥感卫星的飞轮过零规避方法 |
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US3194948A (en) * | 1958-08-07 | 1965-07-13 | Itt | Velocity and position computer |
CN100493993C (zh) * | 2007-12-26 | 2009-06-03 | 北京控制工程研究所 | 一种卫星的自主变轨方法 |
CN100529667C (zh) * | 2007-12-26 | 2009-08-19 | 北京控制工程研究所 | 一种自主恢复轨控故障时的星敏感器定姿方法 |
CN106275508B (zh) * | 2016-08-15 | 2019-03-01 | 上海航天控制技术研究所 | 一种卫星绕空间轴的最短路径姿态机动控制方法 |
CN107450582B (zh) * | 2017-08-22 | 2020-07-03 | 长光卫星技术有限公司 | 一种基于星上实时规划的相控阵数传引导控制方法 |
CN107389098B (zh) * | 2017-08-22 | 2019-07-26 | 长光卫星技术有限公司 | 一种航天器星敏感器安装矩阵在轨标定方法 |
CN108279010A (zh) * | 2017-12-18 | 2018-07-13 | 北京时代民芯科技有限公司 | 一种基于多传感器的微小卫星姿态确定方法 |
DE102018118673B3 (de) * | 2018-08-01 | 2019-12-05 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Vorrichtung und Verfahren zum Identifizieren einer Trägheitsmatrix eines Raumfahrzeugs |
CN109459065B (zh) * | 2018-12-26 | 2020-06-19 | 长光卫星技术有限公司 | 一种基于卫星惯性空间旋转姿态的陀螺安装矩阵标定方法 |
CN110109470B (zh) * | 2019-04-09 | 2021-10-29 | 西安电子科技大学 | 基于无迹卡尔曼滤波的联合定姿方法、卫星姿态控制系统 |
CN110329545B (zh) * | 2019-07-15 | 2020-10-23 | 北京控制工程研究所 | 一种基于滤波平滑的闭环控制系统姿态引入修正方法 |
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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. 1299, Mingxi Road, Beihu science and Technology Development Zone, Changchun City, Jilin Province Patentee before: CHANG GUANG SATELLITE TECHNOLOGY Co.,Ltd. |
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Denomination of invention: A nonlinear filtering method for attitude determination of remote sensing satellites Effective date of registration: 20220720 Granted publication date: 20220215 Pledgee: National Development Bank of China Jilin branch Pledgor: Changguang Satellite Technology Co.,Ltd. Registration number: Y2022220000041 |