新型分体式星敏感器设计及其应用

钟红军; 卢欣; 李春江; 李玉明; 李晓

留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

新型分体式星敏感器设计及其应用

钟红军, 卢欣, 李春江, 李玉明, 李晓

文章导航 > 红外与激光工程 > 2014 > 43(4): 1278-1283

钟红军, 卢欣, 李春江, 李玉明, 李晓. 新型分体式星敏感器设计及其应用[J]. 红外与激光工程, 2014, 43(4): 1278-1283.

引用本文:

钟红军, 卢欣, 李春江, 李玉明, 李晓. 新型分体式星敏感器设计及其应用[J]. 红外与激光工程, 2014, 43(4): 1278-1283.

Zhong Hongjun, Lu Xin, Li Chunjiang, Li Yuming, Li Xiao. Design and applications of novel separated type star tracker[J]. Infrared and Laser Engineering, 2014, 43(4): 1278-1283.

Citation:

Zhong Hongjun, Lu Xin, Li Chunjiang, Li Yuming, Li Xiao. Design and applications of novel separated type star tracker[J]. Infrared and Laser Engineering, 2014, 43(4): 1278-1283.

新型分体式星敏感器设计及其应用

1.
北京控制工程研究所,北京100190

详细信息

作者简介:
钟红军（1978- ），男，博士，高级工程师，主要从事星敏感器设计及测试验证等方面的研究。Email：mailzonecn@163.com

中图分类号: V448.22

Design and applications of novel separated type star tracker

1.
Beijing Institute of Control Engineering,Beijing 100190,China

摘要: 星敏感器是当前广泛应用于航天器姿态测量的高精度光学姿态敏感器。介绍了一种新型分体式星敏感器的总体设计、应用及验证情况，其已成功应用于科学试验、通讯及地球观测等多种卫星平台，共有21套产品在轨验证。根据在轨遥测数据分析，全面验证了其主要技术指标：探测灵敏度5.7Mv、数据更新率8Hz、测量精度2.6、阳光抑制角28、动态性能1（）/s等。新型分体式星敏感器是国际上首个在轨飞行验证并引入控制系统闭环控制的APS星敏感器，根据地面测试验证结果和20余套产品长达两年在轨数据的全面分析，其在轨性能与地面测试性能一致，在轨测试结果证明产品的测量精度、鲁棒性、可用性和可靠性等主要性能满足卫星使用要求。
- 新型星敏感器 /
- 分体式 /
- 应用
Abstract: Star tracker is current widely used optical sensor in spacecraft attitude control system which produces the most accurate measurements. The overall design description, application and qualification results of a novel separated autonomous miniature star tracker were introduced. The novel separated type star tracker successfully operated in-orbit on a large variety of different satellite platforms such as scientific experiment, telecommunication and earth observation. The novel star tracker has applied in-orbit with a total of 21 sets of products up to now. According to the real time telemetry data packages under real in-orbit conditions, the main qualification features are sensitivity 5.7 Mv, update rate 8 Hz, accuracy 2.6, sun exclusion 28, tracking slew rate 1 ()/s. The novel separated type star tracker was the first APS based star tracker ever flown which was adopted in AOCS closed loop control. A full analysis on ground qualification campaign was carried out successfully on the novel star tracker and an in-flight qualification was also achieved, with more than two years information from 20 other star trackers on different satellites. In flight results are in accordance with results obtained from ground night sky tests. The analysis results allow an almost complete validation of star tracker major requirements: accuracy, robustness, availability and reliability.
- novel star tracker /
- separated type /
- application

[1]	Tu Shancheng. Attitude Dynamics and Control of Satellite(3)[M]. Beijing: Astronautic Publishing House, 2003: 122-183. (in Chinese) 屠善澄. 卫星姿态动力学与控制(3) [M]. 北京: 宇航出版社, 2003, 122-183.
[2]
[3]
[4]	Liebe C C. Accuracy performance of star tracker-a tutorial[J]. IEEE Transaction on Aerospace and Electronic Systems, 2002, 38(2): 587-599.
[5]
[6]	Liebe C C. Dennison E, Hancock B, et al. Active Pixel Sensor(APS) based star tracker[J]. IEEE, 1998: 119-127.
[7]	Tang Yong, Lu xin, Hao Yuncai. Suppression and analysis of stray light in a star sensor [J]. Aerospace Control, 2004, 22(3): 58-61. (in Chinese) 唐勇, 卢欣, 郝云彩. 星敏感器杂光抑制分析[J]. 航天控制, 2004, 22(3): 58-61.
[8]
[9]	Li Baohua, Chen Xijun, Zheng Xunjiang, et al. Autonomous star tracking algorithm with high dynamic spacecraft [J]. Infrared and Laser Engineering, 2012, 41(1): 190-195. (in Chinese) 李葆华, 陈希军, 郑循江, 等. 星敏感器高动态下自主星跟踪算法[J]. 红外与激光工程, 2012, 41(1): 190-195.
[10]
[11]
[12]	Jiang Jie, Zhang Guangjun, Li Xiao, et al. A fast star tracking algorithm for star sensor [J]. Acta Aeronautica Et Astronautica Sinica, 2006, 27(5): 913-916. (in Chinese) 江洁, 张广军, 李宵, 等. 一种快速的星敏感器星跟踪方法研究[J]. 航空学报, 2006, 27(5): 913-916.
[13]	Jin Yan, Jiang Jie, Zhang Guangjun. Star extraction method for high dynamic star sensor [J]. Infrared and Laser Engineering, 2011, 40(11): 2281-2285. (in Chinese) 金雁, 江洁, 张广军. 高动态星体目标提取方法[J]. 红外与激光工程, 2011, 40(11): 2281-2285.
[14]
[15]	Zhong Hongjun, Yang Mengfei, Lu Xin. Calibration Method of Star Sensor[J]. Acta Optical Sinica, 2010, 30 (5): 1343-1348. (in Chinese) 钟红军, 杨孟飞, 卢欣. 星敏感器标定方法研究[J]. 光学学报, 2010, 30(5): 1343-1348.
[16]
[17]	Qiao Peiyu, He Xin, Wei Zhonghui, et al. Calibration of high-accuracy star sensor [J]. Infrared and Laser Engineering, 2012, 41(10): 2779-2784. (in Chinese) 乔培玉, 何昕, 魏仲慧, 等. 高精度星敏感器的标定[J]. 红外与激光工程, 2012, 41(10): 2779-2784.

[1]	朱嘉康, 安其昌, 杨飞. 大口径望远镜镜面视宁度检测方法综述 . 红外与激光工程, 2023, 52(2): 20220488-1-20220488-18. doi: 10.3788/IRLA20220488
[2]	任平川, 周琦, 金荷, 宋卿争, 缪鹏飞. 星敏感器动态精度评价方法 . 红外与激光工程, 2022, 51(3): 20210571-1-20210571-8. doi: 10.3788/IRLA20210571
[3]	刘巧莉, 刘畅, 王艺潼, 郝凌翔, 黄永清, 胡安琪, 郭霞. 硅单光子探测器研制及其在高精度星地时间比对中应用（特邀） . 红外与激光工程, 2021, 50(1): 20211004-1-20211004-7. doi: 10.3788/IRLA20211004
[4]	冯婕, 李豫东, 文林, 郭旗. CMOS图像传感器辐射损伤导致星敏感器性能退化机理 . 红外与激光工程, 2020, 49(5): 20190555-20190555-7. doi: 10.3788/IRLA20190555
[5]	岳春宇, 郑永超, 邢艳秋, 庞勇, 李世明, 蔡龙涛, 何红艳. 星载激光遥感林业应用发展研究 . 红外与激光工程, 2020, 49(11): 20200235-1-20200235-10. doi: 10.3788/IRLA20200235
[6]	王立, 吴奋陟, 梁潇. 我国深空探测光学敏感器技术发展与应用（特约） . 红外与激光工程, 2020, 49(5): 20201004-20201004-6. doi: 10.3788/IRLA20201004
[7]	白振旭, 杨学宗, 陈晖, 金舵, 丁洁, 齐瑶瑶, 李森森, 闫秀生, 王雨雷, 吕志伟. 高功率金刚石激光技术研究进展（特邀） . 红外与激光工程, 2020, 49(12): 20201076-1-20201076-13. doi: 10.3788/IRLA20201076
[8]	孙明晨, 涂翠, 胡雄, 宫晓艳, 郭文杰. 临近空间星光掩星技术的初步应用 . 红外与激光工程, 2019, 48(9): 909001-0909001(9). doi: 10.3788/IRLA201948.0909001
[9]	王巍. 新型惯性技术发展及在宇航领域的应用 . 红外与激光工程, 2016, 45(3): 301001-0301001(6). doi: 10.3788/IRLA201645.0301001
[10]	杨洋, 刘兵, 赵勇, 王辉, 赵亚丽, 杜瑶. DWDM技术在新型波长解调方法中的应用 . 红外与激光工程, 2016, 45(8): 822007-0822007(7). doi: 10.3788/IRLA201645.0822007
[11]	崔祥祥, 王宏力, 陆敬辉, 乔兴, 邓长智, 张勇, 赵爱罡. 适用于小视场星敏感器的导航星表构建方法 . 红外与激光工程, 2015, 44(4): 1249-1253.
[12]	陈启梦员, 张国玉, 王哲, 王凌云, 高玉军. 甚高精度星敏感器测试用静态星模拟器设计 . 红外与激光工程, 2014, 43(6): 1830-1835.
[13]	陈启梦, 张国玉, 王凌云, 王志海, 孙向阳. 高精度星敏感器测试设备的设计 . 红外与激光工程, 2014, 43(7): 2234-2239.
[14]	江帆, 王忠素, 陈立恒, 吴清文, 郭亮. 星敏感器组件的热设计 . 红外与激光工程, 2014, 43(11): 3740-3745.
[15]	孟合民, 高教波, 郑雅卫, 张磊, 范喆, 骆延令, 李明伟. 基于分体式Sagnac干涉仪的长波红外干涉成像光谱系统 . 红外与激光工程, 2014, 43(1): 19-25.
[16]	王延新, 刘琪, 李兆熠, 张爱珍. 红外成像导引技术应用中若干问题的分析 . 红外与激光工程, 2014, 43(1): 26-32.
[17]	陈聪, 王宏力, 崔祥祥, 陆敬辉, 姜伟. 基于预测跟踪星表提高星敏感器实时性的方法 . 红外与激光工程, 2013, 42(8): 2190-2196.
[18]	孙高飞, 张国玉, 高玉军, 王凌云, 苏拾, 付芸, 王向东. 星敏感器地面标定设备的设计 . 红外与激光工程, 2013, 42(10): 2822-2827.
[19]	任秉文, 金光, 王天聪, 钟兴, 张鹏. 机载全天时星敏感器参数设计及实验 . 红外与激光工程, 2013, 42(4): 1003-1010.
[20]	李葆华, 陈希军, 郑循江, 泮宏梁. 星敏感器高动态下自主星跟踪算法 . 红外与激光工程, 2012, 41(1): 190-195.

点击查看大图

计量

文章访问数: 860
HTML全文浏览量: 68
PDF下载量: 294
被引次数: 0

新型分体式星敏感器设计及其应用

1. 北京控制工程研究所,北京100190

作者简介:
钟红军（1978- ），男，博士，高级工程师，主要从事星敏感器设计及测试验证等方面的研究。Email：mailzonecn@163.com

收稿日期: 2013-08-11
修回日期: 2013-09-20
刊出日期: 2014-04-25

中图分类号: V448.22

关键词:

摘要: 星敏感器是当前广泛应用于航天器姿态测量的高精度光学姿态敏感器。介绍了一种新型分体式星敏感器的总体设计、应用及验证情况，其已成功应用于科学试验、通讯及地球观测等多种卫星平台，共有21套产品在轨验证。根据在轨遥测数据分析，全面验证了其主要技术指标：探测灵敏度5.7Mv、数据更新率8Hz、测量精度2.6、阳光抑制角28、动态性能1（）/s等。新型分体式星敏感器是国际上首个在轨飞行验证并引入控制系统闭环控制的APS星敏感器，根据地面测试验证结果和20余套产品长达两年在轨数据的全面分析，其在轨性能与地面测试性能一致，在轨测试结果证明产品的测量精度、鲁棒性、可用性和可靠性等主要性能满足卫星使用要求。

English Abstract

Design and applications of novel separated type star tracker

1. Beijing Institute of Control Engineering,Beijing 100190,China

Received Date: 2013-08-11
Rev Recd Date: 2013-09-20
Publish Date: 2014-04-25

Keywords:

Abstract: Star tracker is current widely used optical sensor in spacecraft attitude control system which produces the most accurate measurements. The overall design description, application and qualification results of a novel separated autonomous miniature star tracker were introduced. The novel separated type star tracker successfully operated in-orbit on a large variety of different satellite platforms such as scientific experiment, telecommunication and earth observation. The novel star tracker has applied in-orbit with a total of 21 sets of products up to now. According to the real time telemetry data packages under real in-orbit conditions, the main qualification features are sensitivity 5.7 Mv, update rate 8 Hz, accuracy 2.6, sun exclusion 28, tracking slew rate 1 ()/s. The novel separated type star tracker was the first APS based star tracker ever flown which was adopted in AOCS closed loop control. A full analysis on ground qualification campaign was carried out successfully on the novel star tracker and an in-flight qualification was also achieved, with more than two years information from 20 other star trackers on different satellites. In flight results are in accordance with results obtained from ground night sky tests. The analysis results allow an almost complete validation of star tracker major requirements: accuracy, robustness, availability and reliability.