CN107422641B - 复杂约束条件下的航天器编队姿态有限时间协同控制方法 - Google Patents
复杂约束条件下的航天器编队姿态有限时间协同控制方法 Download PDFInfo
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- CN107422641B CN107422641B CN201710742009.3A CN201710742009A CN107422641B CN 107422641 B CN107422641 B CN 107422641B CN 201710742009 A CN201710742009 A CN 201710742009A CN 107422641 B CN107422641 B CN 107422641B
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Classifications
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
- G05B13/042—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators in which a parameter or coefficient is automatically adjusted to optimise the performance
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B13/00—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
- G05B13/02—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
- G05B13/04—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
- G05B13/047—Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators the criterion being a time optimal performance criterion
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
- G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
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- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- General Physics & Mathematics (AREA)
- Computer Vision & Pattern Recognition (AREA)
- Medical Informatics (AREA)
- Software Systems (AREA)
- Evolutionary Computation (AREA)
- Health & Medical Sciences (AREA)
- Artificial Intelligence (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
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CN201710742009.3A CN107422641B (zh) | 2017-08-25 | 2017-08-25 | 复杂约束条件下的航天器编队姿态有限时间协同控制方法 |
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CN201710742009.3A CN107422641B (zh) | 2017-08-25 | 2017-08-25 | 复杂约束条件下的航天器编队姿态有限时间协同控制方法 |
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CN107422641A CN107422641A (zh) | 2017-12-01 |
CN107422641B true CN107422641B (zh) | 2019-06-25 |
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Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
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CN109491381B (zh) * | 2018-11-06 | 2020-10-27 | 中国科学技术大学 | 基于观测器的多移动机器人自适应编队跟踪控制方法 |
CN110110342B (zh) * | 2018-12-11 | 2023-08-25 | 上海航天控制技术研究所 | 一种基于邻近算法的组合体航天器数据驱动控制方法 |
CN109901394B (zh) * | 2019-03-22 | 2021-03-19 | 北京航空航天大学 | 基于分布式高阶滑模估计器的航天器姿态协同控制方法 |
CN110456807B (zh) * | 2019-07-02 | 2021-01-12 | 西北工业大学 | 一种多航天器一致性动态增益控制方法 |
CN110687915B (zh) * | 2019-10-17 | 2021-06-08 | 哈尔滨工业大学 | 一种基于无向通信拓扑的航天器编队姿态协同控制方法 |
CN111442786B (zh) * | 2020-05-21 | 2021-08-20 | 合肥工业大学 | 一种飞行器陀螺仪的零点漂移偏差和姿态估计方法 |
CN111830974A (zh) * | 2020-06-30 | 2020-10-27 | 珠海云洲智能科技有限公司 | 无人船位置分配策略确定方法、装置、设备及存储介质 |
CN112046794B (zh) * | 2020-07-16 | 2022-02-25 | 中国人民解放军军事科学院国防科技创新研究院 | 基于混合高斯模型的固定时间约束的航天器集群控制方法 |
CN111949040B (zh) * | 2020-07-17 | 2021-08-13 | 南京航空航天大学 | 高效利用空间无线资源的卫星编队姿态协同跟踪控制方法 |
CN112000108B (zh) * | 2020-09-08 | 2021-09-21 | 北京航空航天大学 | 一种多智能体集群分组时变编队跟踪控制方法及系统 |
CN113741493B (zh) * | 2021-08-11 | 2023-06-06 | 北京空间飞行器总体设计部 | 一种航天器安全接近控制方法 |
CN116466735B (zh) * | 2023-06-12 | 2023-09-12 | 中南大学 | 一种航天器编队姿态定向协同控制方法及相关设备 |
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US8386098B2 (en) * | 2009-08-03 | 2013-02-26 | David A. Bailey | Method for a deeper search in a time-limited image satellite planning environment |
CN104898691B (zh) * | 2015-04-29 | 2017-07-28 | 哈尔滨工业大学 | 编队卫星有限时间构型包含控制方法 |
CN105138010B (zh) * | 2015-08-31 | 2017-07-28 | 哈尔滨工业大学 | 一种编队卫星分布式有限时间跟踪控制方法 |
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Inventor after: Sun Xiangdong Inventor after: An Xibin Inventor after: Ma Man Inventor after: Liu Gang Inventor after: Xu Jun Inventor after: Zheng Zonggui Inventor after: Wu Liang Inventor after: He Bing Inventor after: Qin Weiwei Inventor after: Zhao Xin Inventor before: Sun Xiangdong Inventor before: Ma Man Inventor before: Liu Gang Inventor before: Xu Jun Inventor before: Zheng Zonggui Inventor before: Wu Liang Inventor before: He Bing Inventor before: Qin Weiwei Inventor before: An Xibin |
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