CN113761664B - 一种遥感卫星成像期间飞轮转速优化方法 - Google Patents
一种遥感卫星成像期间飞轮转速优化方法 Download PDFInfo
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- CN113761664B CN113761664B CN202111079640.2A CN202111079640A CN113761664B CN 113761664 B CN113761664 B CN 113761664B CN 202111079640 A CN202111079640 A CN 202111079640A CN 113761664 B CN113761664 B CN 113761664B
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- 238000003384 imaging method Methods 0.000 title claims abstract description 54
- 238000000034 method Methods 0.000 title claims abstract description 24
- 238000005457 optimization Methods 0.000 title claims abstract description 16
- 238000005259 measurement Methods 0.000 claims description 9
- 238000006243 chemical reaction Methods 0.000 claims description 7
- 238000003032 molecular docking Methods 0.000 claims description 6
- 230000003287 optical effect Effects 0.000 claims description 3
- 230000007704 transition Effects 0.000 claims description 3
- 238000007726 management method Methods 0.000 description 5
- 238000004088 simulation Methods 0.000 description 4
- 230000001105 regulatory effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000036561 sun exposure Effects 0.000 description 1
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
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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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/17—Mechanical parametric or variational design
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/20—Design optimisation, verification or simulation
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F2119/00—Details relating to the type or aim of the analysis or the optimisation
- G06F2119/14—Force analysis or force optimisation, e.g. static or dynamic forces
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Theoretical Computer Science (AREA)
- General Physics & Mathematics (AREA)
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- General Engineering & Computer Science (AREA)
- Computer Hardware Design (AREA)
- Evolutionary Computation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Chemical & Material Sciences (AREA)
- Automation & Control Theory (AREA)
- Computational Mathematics (AREA)
- Mathematical Analysis (AREA)
- Mathematical Optimization (AREA)
- Pure & Applied Mathematics (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
Description
转速 | 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 |
X轴 | 1000 | -1000 | 1000 | 1000 | -1000 | -1000 | 1000 | -1000 |
Y轴 | 1000 | 1000 | -1000 | 1000 | -1000 | 1000 | -1000 | -1000 |
Z轴 | 1000 | 1000 | 1000 | -1000 | 1000 | -1000 | -1000 | -1000 |
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CN116331525B (zh) * | 2023-03-13 | 2024-04-02 | 长光卫星技术股份有限公司 | 一种卫星飞轮转速过零规避方法 |
CN116659543B (zh) * | 2023-06-21 | 2024-05-07 | 中国人民解放军61540部队 | 基于遥感卫星轨道根数的卫星位置姿态估计方法和装置 |
Citations (12)
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US5611505A (en) * | 1994-11-18 | 1997-03-18 | Hughes Electronics | Spacecraft energy storage, attitude steering and momentum management system |
WO2007128112A1 (en) * | 2006-05-08 | 2007-11-15 | Bce Inc. | System and method for unloading angular momentum from a spacecraft momentum wheel stabilization system |
CN101706512A (zh) * | 2009-11-25 | 2010-05-12 | 哈尔滨工业大学 | 基于星敏感器的姿态测量信息和飞轮的角动量测量信息的航天器伪速率的估计方法 |
CN102303708A (zh) * | 2011-06-08 | 2012-01-04 | 哈尔滨工业大学 | 液体回路阀门控制卫星姿态的装置及方法 |
CN103274058A (zh) * | 2013-05-30 | 2013-09-04 | 北京控制工程研究所 | 一种冗余飞轮组角动量自主管理方法 |
CN105005312A (zh) * | 2015-06-29 | 2015-10-28 | 哈尔滨工业大学 | 一种基于最大角加速度和最大角速度卫星规划轨迹方法 |
CN105259794A (zh) * | 2015-11-19 | 2016-01-20 | 中国人民解放军国防科学技术大学 | 一种基于即插即用技术的卫星姿态控制地面仿真*** |
CN107499536A (zh) * | 2017-08-17 | 2017-12-22 | 上海航天控制技术研究所 | 一种偏置动量卫星高精度跟踪控制偏流角的方法 |
CN109460049A (zh) * | 2018-11-14 | 2019-03-12 | 北京控制工程研究所 | 基于惯性指向模式的地球同步轨道卫星远地点变轨方法 |
CN109911248A (zh) * | 2019-03-19 | 2019-06-21 | 湖南航升卫星科技有限公司 | 天基空间运动目标跟踪指向卫星姿态控制方法及*** |
CN111688953A (zh) * | 2020-05-27 | 2020-09-22 | 长光卫星技术有限公司 | 一种光学卫星相控阵数传任务太阳光规避姿态规划方法 |
CN113173267A (zh) * | 2021-04-30 | 2021-07-27 | 北京控制工程研究所 | 一种冗余飞轮组的动态力矩分配与角动量跟踪控制方法 |
-
2021
- 2021-09-15 CN CN202111079640.2A patent/CN113761664B/zh active Active
Patent Citations (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5611505A (en) * | 1994-11-18 | 1997-03-18 | Hughes Electronics | Spacecraft energy storage, attitude steering and momentum management system |
WO2007128112A1 (en) * | 2006-05-08 | 2007-11-15 | Bce Inc. | System and method for unloading angular momentum from a spacecraft momentum wheel stabilization system |
CN101706512A (zh) * | 2009-11-25 | 2010-05-12 | 哈尔滨工业大学 | 基于星敏感器的姿态测量信息和飞轮的角动量测量信息的航天器伪速率的估计方法 |
CN102303708A (zh) * | 2011-06-08 | 2012-01-04 | 哈尔滨工业大学 | 液体回路阀门控制卫星姿态的装置及方法 |
CN103274058A (zh) * | 2013-05-30 | 2013-09-04 | 北京控制工程研究所 | 一种冗余飞轮组角动量自主管理方法 |
CN105005312A (zh) * | 2015-06-29 | 2015-10-28 | 哈尔滨工业大学 | 一种基于最大角加速度和最大角速度卫星规划轨迹方法 |
CN105259794A (zh) * | 2015-11-19 | 2016-01-20 | 中国人民解放军国防科学技术大学 | 一种基于即插即用技术的卫星姿态控制地面仿真*** |
CN107499536A (zh) * | 2017-08-17 | 2017-12-22 | 上海航天控制技术研究所 | 一种偏置动量卫星高精度跟踪控制偏流角的方法 |
CN109460049A (zh) * | 2018-11-14 | 2019-03-12 | 北京控制工程研究所 | 基于惯性指向模式的地球同步轨道卫星远地点变轨方法 |
CN109911248A (zh) * | 2019-03-19 | 2019-06-21 | 湖南航升卫星科技有限公司 | 天基空间运动目标跟踪指向卫星姿态控制方法及*** |
CN111688953A (zh) * | 2020-05-27 | 2020-09-22 | 长光卫星技术有限公司 | 一种光学卫星相控阵数传任务太阳光规避姿态规划方法 |
CN113173267A (zh) * | 2021-04-30 | 2021-07-27 | 北京控制工程研究所 | 一种冗余飞轮组的动态力矩分配与角动量跟踪控制方法 |
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Denomination of invention: A method for optimizing flywheel speed during remote sensing satellite imaging Granted publication date: 20240130 Pledgee: Jilin Chuncheng Rural Commercial Bank Co.,Ltd. Pledgor: Changguang Satellite Technology Co.,Ltd. Registration number: Y2024220000054 |