CN107422641A - 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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- CN107422641A CN107422641A CN201710742009.3A CN201710742009A CN107422641A CN 107422641 A CN107422641 A CN 107422641A CN 201710742009 A CN201710742009 A CN 201710742009A CN 107422641 A CN107422641 A CN 107422641A
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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
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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
- G05B13/047—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
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- 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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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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CN107422641B CN107422641B (zh) | 2019-06-25 |
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Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109491381A (zh) * | 2018-11-06 | 2019-03-19 | 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 |
CN109901394A (zh) * | 2019-03-22 | 2019-06-18 | 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 |
CN110110342A (zh) * | 2018-12-11 | 2019-08-09 | 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 |
CN110456807A (zh) * | 2019-07-02 | 2019-11-15 | 西北工业大学 | 一种多航天器一致性动态增益控制方法 |
CN110687915A (zh) * | 2019-10-17 | 2020-01-14 | 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 |
CN111442786A (zh) * | 2020-05-21 | 2020-07-24 | 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 |
CN111949040A (zh) * | 2020-07-17 | 2020-11-17 | 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 |
CN112000108A (zh) * | 2020-09-08 | 2020-11-27 | 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 |
CN112046794A (zh) * | 2020-07-16 | 2020-12-08 | 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 |
CN112363502A (zh) * | 2020-06-30 | 2021-02-12 | 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 |
CN113741493A (zh) * | 2021-08-11 | 2021-12-03 | 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 |
CN116466735A (zh) * | 2023-06-12 | 2023-07-21 | 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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US20110025554A1 (en) * | 2009-08-03 | 2011-02-03 | Bailey David A | Method for a deeper search in a time-limited image satellite planning environment |
CN104898691A (zh) * | 2015-04-29 | 2015-09-09 | 哈尔滨工业大学 | 编队卫星有限时间构型包含控制方法 |
CN105138010A (zh) * | 2015-08-31 | 2015-12-09 | 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 |
-
2017
- 2017-08-25 CN CN201710742009.3A patent/CN107422641B/zh not_active Expired - Fee Related
Patent Citations (3)
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US20110025554A1 (en) * | 2009-08-03 | 2011-02-03 | Bailey David A | Method for a deeper search in a time-limited image satellite planning environment |
CN104898691A (zh) * | 2015-04-29 | 2015-09-09 | 哈尔滨工业大学 | 编队卫星有限时间构型包含控制方法 |
CN105138010A (zh) * | 2015-08-31 | 2015-12-09 | 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 |
Non-Patent Citations (1)
Title |
---|
傅敬博: "通讯受限条件下航天器编队姿态协同控制方法研究", 《中国优秀硕士学位论文全文数据库(电子期刊) 工科科技II辑》 * |
Cited By (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109491381A (zh) * | 2018-11-06 | 2019-03-19 | 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 |
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 |
CN110110342A (zh) * | 2018-12-11 | 2019-08-09 | 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 |
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 |
CN109901394A (zh) * | 2019-03-22 | 2019-06-18 | 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 |
CN110456807A (zh) * | 2019-07-02 | 2019-11-15 | 西北工业大学 | 一种多航天器一致性动态增益控制方法 |
CN110687915A (zh) * | 2019-10-17 | 2020-01-14 | 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 |
CN111442786A (zh) * | 2020-05-21 | 2020-07-24 | 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 |
CN112363502B (zh) * | 2020-06-30 | 2021-10-08 | 珠海云洲智能科技股份有限公司 | 无人船位置分配策略确定方法、装置、设备及存储介质 |
CN112363502A (zh) * | 2020-06-30 | 2021-02-12 | 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 |
CN112046794A (zh) * | 2020-07-16 | 2020-12-08 | 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 |
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 |
CN111949040A (zh) * | 2020-07-17 | 2020-11-17 | 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 |
CN112000108A (zh) * | 2020-09-08 | 2020-11-27 | 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 |
CN113741493A (zh) * | 2021-08-11 | 2021-12-03 | 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 |
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 |
CN116466735A (zh) * | 2023-06-12 | 2023-07-21 | 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 |
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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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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