CN101712381A - Multi-sensor-based attitude determination system - Google Patents
Multi-sensor-based attitude determination system Download PDFInfo
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- CN101712381A CN101712381A CN200910237658A CN200910237658A CN101712381A CN 101712381 A CN101712381 A CN 101712381A CN 200910237658 A CN200910237658 A CN 200910237658A CN 200910237658 A CN200910237658 A CN 200910237658A CN 101712381 A CN101712381 A CN 101712381A
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Cited By (16)
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CN102156478A (en) * | 2010-12-28 | 2011-08-17 | 北京航空航天大学 | Integrated attitude determination method based on ant colony unscented particle filter algorithm |
CN102494687A (en) * | 2011-10-19 | 2012-06-13 | 清华大学 | High-precision posture/track integrated measurement device |
CN103324583A (en) * | 2013-07-02 | 2013-09-25 | 浙江大学 | Offline high-speed fiber-optic gyroscope data acquisition method |
CN103438879A (en) * | 2013-09-02 | 2013-12-11 | 北京航空航天大学 | Atomic spin gyroscope and magnetometer tightly-integrated attitude determination method based on ant colony PF (Particle Filter) algorithm |
CN104118578A (en) * | 2014-06-24 | 2014-10-29 | 上海微小卫星工程中心 | Micro-satellite platform multi-sensor data dynamic fusing system and method |
CN104765667A (en) * | 2015-04-17 | 2015-07-08 | 西安电子科技大学 | FPGA program fragile branch obtaining method based on ant colony optimization |
CN104977941A (en) * | 2014-04-02 | 2015-10-14 | 波音公司 | Localization within an environment using sensor fusion |
CN108313329A (en) * | 2018-04-03 | 2018-07-24 | 上海微小卫星工程中心 | A kind of satellite platform data dynamic fusion system and method |
CN109186588A (en) * | 2018-10-10 | 2019-01-11 | 上海航天控制技术研究所 | A kind of miniature multimode star sensor |
CN109598718A (en) * | 2018-12-06 | 2019-04-09 | 余姚市华耀工具科技有限公司 | Equipment replacement demand analysis mechanism |
CN109945854A (en) * | 2019-03-26 | 2019-06-28 | 上海微小卫星工程中心 | A method of star sensor data is merged based on quaternary number difference |
CN111156992A (en) * | 2019-12-31 | 2020-05-15 | 中国船舶重工集团公司第七一七研究所 | Miniature satellite-borne star sensor and working process time sequence thereof |
CN111332501A (en) * | 2020-02-26 | 2020-06-26 | 上海航天控制技术研究所 | Multi-control and multi-reference design method of satellite attitude control system |
CN111895993A (en) * | 2020-08-04 | 2020-11-06 | 上海航天控制技术研究所 | Miniature star sensor circuit system |
CN113607155A (en) * | 2021-07-12 | 2021-11-05 | 上海卫星工程研究所 | Intelligent multiplexing method and system for sensors under multi-star assembly |
CN113710579A (en) * | 2019-03-25 | 2021-11-26 | 空客防务与空间有限公司 | Device and method for determining the attitude of a satellite equipped with a gyroscopic actuator and satellite carrying such a device |
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DE4129630A1 (en) * | 1991-09-06 | 1993-05-06 | Deutsche Aerospace Ag, 8000 Muenchen, De | MEASURING ARRANGEMENT AND CONTROL SYSTEM FOR THE POSITION CONTROL OF A THREE-AXIS-STABILIZED SATELLITE AND RELATED MEASURING AND CONTROL PROCEDURES |
US6272432B1 (en) * | 1999-05-10 | 2001-08-07 | Hughes Electronics Corporation | System and method for correcting star tracker low spatial frequency error in stellar-inertial attitude determination systems |
US6702234B1 (en) * | 2002-03-29 | 2004-03-09 | Lockheed Martin Corporation | Fault tolerant attitude control system for zero momentum spacecraft |
CN100356139C (en) * | 2005-01-21 | 2007-12-19 | 清华大学 | Miniature assembled gesture measuring system for mini-satellite |
CN100348461C (en) * | 2006-08-01 | 2007-11-14 | 北京航空航天大学 | High precision APS sun sensor |
CN100487618C (en) * | 2007-06-08 | 2009-05-13 | 北京航空航天大学 | High precision combined posture-determining method based on optimally genetic REQUEST and GUPF |
CN100538276C (en) * | 2007-11-16 | 2009-09-09 | 北京航空航天大学 | A kind of MEMS gyroscopes error compensation method for micro satellite based on integrated neural network |
CN101513939B (en) * | 2009-04-03 | 2011-01-05 | 北京航空航天大学 | Two dimentional attitude control system of synthetic aperture radar satellite |
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2009
- 2009-11-13 CN CN 200910237658 patent/CN101712381B/en not_active Expired - Fee Related
Cited By (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102156478A (en) * | 2010-12-28 | 2011-08-17 | 北京航空航天大学 | Integrated attitude determination method based on ant colony unscented particle filter algorithm |
CN102156478B (en) * | 2010-12-28 | 2013-11-06 | 北京航空航天大学 | Integrated attitude determination method based on ant colony unscented particle filter algorithm |
CN102494687A (en) * | 2011-10-19 | 2012-06-13 | 清华大学 | High-precision posture/track integrated measurement device |
CN102494687B (en) * | 2011-10-19 | 2013-09-04 | 清华大学 | High-precision posture/track integrated measurement device |
CN103324583A (en) * | 2013-07-02 | 2013-09-25 | 浙江大学 | Offline high-speed fiber-optic gyroscope data acquisition method |
CN103324583B (en) * | 2013-07-02 | 2016-03-02 | 浙江大学 | A kind of optical fibre gyro off-line High Speed Data Collection Method |
CN103438879A (en) * | 2013-09-02 | 2013-12-11 | 北京航空航天大学 | Atomic spin gyroscope and magnetometer tightly-integrated attitude determination method based on ant colony PF (Particle Filter) algorithm |
CN104977941B (en) * | 2014-04-02 | 2019-04-30 | 波音公司 | The device and method of mobile platform are guided in environment |
CN104977941A (en) * | 2014-04-02 | 2015-10-14 | 波音公司 | Localization within an environment using sensor fusion |
CN104118578A (en) * | 2014-06-24 | 2014-10-29 | 上海微小卫星工程中心 | Micro-satellite platform multi-sensor data dynamic fusing system and method |
CN104118578B (en) * | 2014-06-24 | 2016-02-03 | 上海微小卫星工程中心 | A kind of microsatellite platform multiple sensor data dynamic fusion system and method |
CN104765667B (en) * | 2015-04-17 | 2018-09-28 | 西安电子科技大学 | A kind of FPGA program fragility branch acquiring methods based on ant group algorithm |
CN104765667A (en) * | 2015-04-17 | 2015-07-08 | 西安电子科技大学 | FPGA program fragile branch obtaining method based on ant colony optimization |
CN108313329A (en) * | 2018-04-03 | 2018-07-24 | 上海微小卫星工程中心 | A kind of satellite platform data dynamic fusion system and method |
CN109186588A (en) * | 2018-10-10 | 2019-01-11 | 上海航天控制技术研究所 | A kind of miniature multimode star sensor |
CN109598718B (en) * | 2018-12-06 | 2020-12-04 | 安徽省华腾农业科技有限公司经开区分公司 | Equipment replacement demand analysis mechanism |
CN109598718A (en) * | 2018-12-06 | 2019-04-09 | 余姚市华耀工具科技有限公司 | Equipment replacement demand analysis mechanism |
CN113710579A (en) * | 2019-03-25 | 2021-11-26 | 空客防务与空间有限公司 | Device and method for determining the attitude of a satellite equipped with a gyroscopic actuator and satellite carrying such a device |
CN109945854A (en) * | 2019-03-26 | 2019-06-28 | 上海微小卫星工程中心 | A method of star sensor data is merged based on quaternary number difference |
CN111156992A (en) * | 2019-12-31 | 2020-05-15 | 中国船舶重工集团公司第七一七研究所 | Miniature satellite-borne star sensor and working process time sequence thereof |
CN111332501A (en) * | 2020-02-26 | 2020-06-26 | 上海航天控制技术研究所 | Multi-control and multi-reference design method of satellite attitude control system |
CN111332501B (en) * | 2020-02-26 | 2021-08-10 | 上海航天控制技术研究所 | Multi-control and multi-reference design method of satellite attitude control system |
CN111895993A (en) * | 2020-08-04 | 2020-11-06 | 上海航天控制技术研究所 | Miniature star sensor circuit system |
CN111895993B (en) * | 2020-08-04 | 2023-02-03 | 上海航天控制技术研究所 | Miniature star sensor circuit system |
CN113607155A (en) * | 2021-07-12 | 2021-11-05 | 上海卫星工程研究所 | Intelligent multiplexing method and system for sensors under multi-star assembly |
CN113607155B (en) * | 2021-07-12 | 2023-10-10 | 上海卫星工程研究所 | Intelligent multiplexing method and system for sensors under multi-star combination |
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Inventor after: Quan Wei Inventor after: Guo Lei Inventor after: Fang Jiancheng Inventor after: Xu Liang Inventor after: Liu Bingli Inventor after: Yang Zhaohua Inventor before: Guo Lei Inventor before: Quan Wei Inventor before: Liu Bingli Inventor before: Yang Zhaohua |
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Free format text: CORRECT: INVENTOR; FROM: GUO LEI QUAN WEI LIU BINGLI YANG ZHAOHUA TO: QUAN WEI GUO LEI FANG JIANCHENG XU LIANG LIU BINGLI YANG ZHAOHUA |
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