CN111232248A - 一种基于轨控推力器脉宽调制的姿轨一体化控制方法 - Google Patents
一种基于轨控推力器脉宽调制的姿轨一体化控制方法 Download PDFInfo
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- CN111232248A CN111232248A CN202010093480.6A CN202010093480A CN111232248A CN 111232248 A CN111232248 A CN 111232248A CN 202010093480 A CN202010093480 A CN 202010093480A CN 111232248 A CN111232248 A CN 111232248A
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- thruster
- attitude
- control
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- 238000000034 method Methods 0.000 title claims abstract description 13
- 238000005259 measurement Methods 0.000 claims description 3
- 230000000694 effects Effects 0.000 abstract description 2
- 230000036544 posture Effects 0.000 abstract 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
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Classifications
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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
- B64G1/242—Orbits and trajectories
-
- 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
-
- 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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- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Description
推力器T1 | 0,sin(15°),-cos(15°) |
推力器T2 | 0,sin(15°),-cos(15°) |
推力器T3 | 0,-sin(15°),-cos(15°) |
推力器T4 | 0,-sin(15°),-cos(15°) |
力矩方向 | 推力器组合 |
+X | T3+T4 |
-X | T1+T2 |
+Y | T1+T4 |
-Y | T2+T3 |
+Z | T1+T3 |
-Z | T2+T4 |
Claims (5)
Priority Applications (1)
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CN202010093480.6A CN111232248B (zh) | 2020-02-14 | 2020-02-14 | 一种基于轨控推力器脉宽调制的姿轨一体化控制方法 |
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CN202010093480.6A CN111232248B (zh) | 2020-02-14 | 2020-02-14 | 一种基于轨控推力器脉宽调制的姿轨一体化控制方法 |
Publications (2)
Publication Number | Publication Date |
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CN111232248A true CN111232248A (zh) | 2020-06-05 |
CN111232248B CN111232248B (zh) | 2021-07-27 |
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CN202010093480.6A Active CN111232248B (zh) | 2020-02-14 | 2020-02-14 | 一种基于轨控推力器脉宽调制的姿轨一体化控制方法 |
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CN (1) | CN111232248B (zh) |
Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5439191A (en) * | 1993-02-16 | 1995-08-08 | Board Of Regents, The University Of Texas System | Railgun thruster |
CN1148836A (zh) * | 1994-03-30 | 1997-04-30 | 法国国家太空研究中心 | 装有磁矩和空气动力矩发生器的人造卫星及该卫星的控制方法 |
EP0818721A1 (en) * | 1996-07-10 | 1998-01-14 | HE HOLDINGS, INC. dba HUGHES ELECTRONICS | Method and apparatus for a satellite station keeping |
CN1206671A (zh) * | 1997-07-25 | 1999-02-03 | 航空发动机的结构和研究公司 | 小型人造卫星的紧凑的单一推进剂单元推进系统 |
EP1852350A1 (en) * | 2006-05-03 | 2007-11-07 | Eutelsat | Method of operating a geostationary satellite and satellite control system for implementing said method |
CN101214859A (zh) * | 2007-12-26 | 2008-07-09 | 北京控制工程研究所 | 一种变轨期间自主故障检测恢复控制的方法 |
CN101695961A (zh) * | 2009-11-02 | 2010-04-21 | 哈尔滨工业大学 | 一种基于执行机构归一化可达集顶点的控制分配方法 |
CN102649480A (zh) * | 2012-04-23 | 2012-08-29 | 上海卫星工程研究所 | 一种可全向变轨航天器的16推力器布局设计方法 |
CN104590587A (zh) * | 2014-11-27 | 2015-05-06 | 哈尔滨工业大学 | 基于时间配比的卫星三轴控制力矩解耦的实现方法 |
CN104932261A (zh) * | 2015-05-26 | 2015-09-23 | 南京航空航天大学 | 姿轨一体卫星的推力分配方法 |
CN105620792A (zh) * | 2016-02-05 | 2016-06-01 | 上海微小卫星工程中心 | 一种采用斜装推力器进行卫星姿态和轨道控制的方法 |
CN105892478A (zh) * | 2016-06-29 | 2016-08-24 | 哈尔滨工业大学 | 一种面向姿轨一体化控制的多执行机构协同控制分配方法 |
CN107600462A (zh) * | 2017-08-22 | 2018-01-19 | 长光卫星技术有限公司 | 一种基于时分复用方式的小卫星轨道控制方法 |
-
2020
- 2020-02-14 CN CN202010093480.6A patent/CN111232248B/zh active Active
Patent Citations (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5439191A (en) * | 1993-02-16 | 1995-08-08 | Board Of Regents, The University Of Texas System | Railgun thruster |
CN1148836A (zh) * | 1994-03-30 | 1997-04-30 | 法国国家太空研究中心 | 装有磁矩和空气动力矩发生器的人造卫星及该卫星的控制方法 |
EP0818721A1 (en) * | 1996-07-10 | 1998-01-14 | HE HOLDINGS, INC. dba HUGHES ELECTRONICS | Method and apparatus for a satellite station keeping |
CN1206671A (zh) * | 1997-07-25 | 1999-02-03 | 航空发动机的结构和研究公司 | 小型人造卫星的紧凑的单一推进剂单元推进系统 |
EP1852350A1 (en) * | 2006-05-03 | 2007-11-07 | Eutelsat | Method of operating a geostationary satellite and satellite control system for implementing said method |
CN101214859A (zh) * | 2007-12-26 | 2008-07-09 | 北京控制工程研究所 | 一种变轨期间自主故障检测恢复控制的方法 |
CN101695961A (zh) * | 2009-11-02 | 2010-04-21 | 哈尔滨工业大学 | 一种基于执行机构归一化可达集顶点的控制分配方法 |
CN102649480A (zh) * | 2012-04-23 | 2012-08-29 | 上海卫星工程研究所 | 一种可全向变轨航天器的16推力器布局设计方法 |
CN104590587A (zh) * | 2014-11-27 | 2015-05-06 | 哈尔滨工业大学 | 基于时间配比的卫星三轴控制力矩解耦的实现方法 |
CN104932261A (zh) * | 2015-05-26 | 2015-09-23 | 南京航空航天大学 | 姿轨一体卫星的推力分配方法 |
CN105620792A (zh) * | 2016-02-05 | 2016-06-01 | 上海微小卫星工程中心 | 一种采用斜装推力器进行卫星姿态和轨道控制的方法 |
CN105892478A (zh) * | 2016-06-29 | 2016-08-24 | 哈尔滨工业大学 | 一种面向姿轨一体化控制的多执行机构协同控制分配方法 |
CN107600462A (zh) * | 2017-08-22 | 2018-01-19 | 长光卫星技术有限公司 | 一种基于时分复用方式的小卫星轨道控制方法 |
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CN111232248B (zh) | 2021-07-27 |
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Effective date of registration: 20240428 Address after: Room 601, Building A-3, Hunan Media Art Industrial Park, No. 601 Dongfanghong North Road, High tech Development Zone, Changsha City, Hunan Province, 410200 Patentee after: Hunan Lanyue Mechanical and Electrical Technology Co.,Ltd. Country or region after: China Address before: 150001 No. 92 West straight street, Nangang District, Heilongjiang, Harbin Patentee before: HARBIN INSTITUTE OF TECHNOLOGY Country or region before: China |
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