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Design of attitude control system for ASRTU microsatellite
- Optics and Precision Engineering Vol. 28, Issue 10, Pages: 2192-2202(2020)
- 作者机构：
1.哈尔滨工业大学 卫星技术研究所, 黑龙江 哈尔滨 150006
2.哈尔滨工业大学(深圳) 空间科学与应用技术研究院, 广东 深圳 518055
- 作者简介：
- 基金信息：
DOI：10.37188/OPE.20202810.2192
CLC： V448.22Received：10 April 2020，
Revised：22 May 2020，
Accepted：22 May 2020，
Published：25 October 2020
- 稿件说明：
移动端阅览
Feng WANG, Shi-bo NIU, Cheng-fei YUE, et al. Design of attitude control system for ASRTU microsatellite[J]. Optics and precision engineering, 2020, 28(10): 2192-2202.
Feng WANG, Shi-bo NIU, Cheng-fei YUE, et al. Design of attitude control system for ASRTU microsatellite[J]. Optics and precision engineering, 2020, 28(10): 2192-2202. DOI： 10.37188/OPE.20202810.2192.
摘要
阿斯图微卫星是一颗由哈尔滨工业大学牵头研制，在中俄工科大学联盟（ASRTU）合作框架下研制的一颗12U立方星，本文针对阿斯图微卫星任务进行了姿态控制系统设计及仿真分析。首先介绍了阿斯图微卫星的控制指标，通过指标分解确定了姿态敏感器及执行机构的主要性能指标。接着，根据星上敏感器的配置情况，设计了多种定姿和控制方案，并对各控制模式间的切换逻辑进行了设计。卫星姿态确定采用了基于陀螺和星敏感器的扩展卡尔曼滤波算法，姿态控制采用了偏差四元数和偏差角速度反馈的PD控制方法。仿真结果表明:星敏感器有效时，姿态确定精度优于20"，姿态指向精度优于0.05°，稳定度优于0.01（°）/s，能够满足阿斯图立方星的任务要求。
Abstract
The ASRTU Microsatellite is a 12U CubeSat managed by the Harbin Institute of Technology and developed under the cooperation of the China-Russia University of Technology Alliance (ASRTU). This paper presents the design of an attitude control system for the ASRTU microsatellite mission. The control indicators of the ASRTU Microsatellite are first introduced and the main performance indicators of the attitude sensor and actuator are determined through index decomposition. Then
according to the configuration of the on-board sensor
a variety of positioning and control scheme designs are presented
and the switching logic between each control mode is described.The extended Kalman filter algorithm based on gyro and star sensors was used for satellite attitude determination
and the deviation quaternion and the deviation angular velocity feedback PD control method was used for attitude control. Simulation results indicate that the accuracy of attitude determination system when the star sensor is valid is better than 20". Moreover
the control accuracy and stability are better than 0.05° and 0.01 (°)/s
respectively.The results indicate that the proposed design meets the mission requirements of ASRTU CubeSat.
关键词
Keywords
references
张 华 , 尹 玉明 , 王 喜奎 . 国外微小卫星发展现状及产品保证研究 . 中国航天 , 2018 . ( 6 ): 51 - 54 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201806013 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201806013 .
H ZHANG , Y M YIN , X K WANG . Study on the overseas microsatellite development status and product warranty . Aerospace China , 2018 . ( 6 ): 51 - 54 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201806013 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201806013 .
J R KOPACZ , R HERSCHITZ , J RONEY . Small satellites an overview and assessment . Acta Astronautica , 2020 . 170 93 - 105 . DOI: 10.1016/j.actaastro.2020.01.034 http://doi.org/10.1016/j.actaastro.2020.01.034 .
姚 云升 . 现代小卫星技术的发展趋向及应用研究 . 科技与创新 , 2019 . ( 2 ): 158 - 159 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=wjsjxx201902078 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=wjsjxx201902078 .
Y SH YAO . Research on Development Trend and Application of Modern Small Satellite Technology . Innovation Science and Technology , 2019 . ( 2 ): 158 - 159 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=wjsjxx201902078 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=wjsjxx201902078 .
林 来兴 . 微小卫星技术发展和应用前景 . 国际太空 , 2019 . ( 6 ): 46 - 48 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=gjtk201906012 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=gjtk201906012 .
L X LIN . Micro satellite technology development and application prospects . Space International , 2019 . ( 6 ): 46 - 48 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=gjtk201906012 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=gjtk201906012 .
YOSHIDA K, YONETOKU D, ARIMOTO M, et al .. Kanazawa-SAT.3: micro-satellite mission for monitoring X-ray transients coincide with gravitational wave events[C]. SPIE Astronomical Telescopes + Instrumentation. Proc SPIE 10699, Space Telescopes and Instrumentation 2018: Ultraviolet to Gamma Ray, Austin, Texas, USA . 2018, 1069: 1069962.
曹明玉. LEO对地观测微小卫星磁姿态控制方法研究[D].哈尔滨: 哈尔滨工业大学, 2017.
CAO M Y. Research on Magnetic Attitude Control Methods of Earth Observation Micro Satellite in Low Earth Orbit [D]. Harbin: Harbin Institute of Technology, 2017.(in Chinese)
李 东 , 朱 振才 , 张 锐 , 等 . SZ-7伴星姿态控制系统设计及在轨试验 . 宇航学报 , 2011 . 32 ( 3 ): 495 - 501 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201103007 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201103007 .
D LI , ZH C ZHU , R ZHANG , 等 . The design and in-orbit test of the companion microsatellite attitude control system in SZ-7 flight mission . Journal of Astronautics , 2011 . 32 ( 3 ): 495 - 501 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201103007 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=yhxb201103007 .
SAKAI S I, FUKUSHIMA Y, SAITO H. Design and on-orbit evaluation of magnetic attitude control system for the "REIMEI" microsatellite[C].2008 10 th IEEE International Workshop on Advanced Motion Control . March 26-28, 2008, Trento , Italy . IEEE , 2008: 584-589.
刘 善伍 , 万 松 , 容 建刚 . 航天器空间环境干扰力矩分析与仿真研究 . 航天控制 , 2015 . 33 ( 2 ): 78 - 81, 92 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=htkz201502014 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=htkz201502014 .
SH W LIU , S WAN , J G RONG . The analysis and simulation of aircraft space environment disturbance torque . Aerospace Control , 2015 . 33 ( 2 ): 78 - 81, 92 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=htkz201502014 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=htkz201502014 .
徐 喆垚 , 陈 宇坤 , 张 义超 , 等 . LH-2微小卫星综合电子系统设计及姿态控制研究 . 载人航天 , 2020 . 26 ( 1 ): 88 - 93, 81 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zrht202001013 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zrht202001013 .
ZH Y XU , Y K CHEN , Y C ZHANG , 等 . Study on integrated electrical system design and attitude control of microsatellite LH-2 . Manned Spaceflight , 2020 . 26 ( 1 ): 88 - 93, 81 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zrht202001013 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zrht202001013 .
王 谦 , 李 新洪 , 贺 广松 , 等 . 基于EKF的航天器姿态确定算法及精度分析 . 计算机测量与控制 , 2018 . 26 ( 6 ): 155 - 159 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jsjzdclykz201806040 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jsjzdclykz201806040 .
Q WANG , X H LI , G S HE , 等 . Spacecraft attitude determination algorithm and precision analysis based on EKF . Computer Measurement & Control , 2018 . 26 ( 6 ): 155 - 159 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jsjzdclykz201806040 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jsjzdclykz201806040 .
宋亮.星敏感器陀螺姿态确定系统在轨标定研究[D].哈尔滨: 哈尔滨工业大学, 2011.
SONG L. Research on In-orbit Calibration Methods for Star Tracker-gyro Attitude Determination System [D]. Harbin: Harbin Institute of Technology, 2011.(in Chinese)
陈 雪芹 , 耿 云海 . 陀螺/星敏感器在轨标定算法研究 . 哈尔滨工业大学学报 , 2006 . 38 ( 8 ): 1369 - 1373 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgydxxb200608043 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgydxxb200608043 .
X Q CHEN , Y H GENG . On-orbit calibration algorithm for gyros/star sensor . Journal of Harbin Institute of Technology , 2006 . 38 ( 8 ): 1369 - 1373 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgydxxb200608043 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hebgydxxb200608043 .
陈 雪芹 , 耿 云海 . 一种利用星敏感器对陀螺进行在轨标定的算法 . 系统工程与电子技术 , 2005 . 27 ( 12 ): 2112 - 2116 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xtgcydzjs200512038 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xtgcydzjs200512038 .
X Q CHEN , Y H GENG . On-orbit calibration algorithm with star sensors of gyros . Systems Engineering and Electronics , 2005 . 27 ( 12 ): 2112 - 2116 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xtgcydzjs200512038 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xtgcydzjs200512038 .
陶子英.姿态测量仪表在轨标定技术[D].哈尔滨: 哈尔滨工业大学, 2014.
TAO Z Y. On-orbit calibration technology of attitude measurement instruments [D]. Harbin: Harbin Institute of Technology, 2014.(in Chinese)
FAN W. Nano Satellite Attitude Estimation with Magnetometer and Photodiodes Measurements[C]. 28th China Control and Decision Conference. Yinchuan: Editorial Department of Control and Decision , 2016: 1866-1870.
马星宇.基于反作用飞轮和磁力矩器的卫星姿态控制系统研究[D].哈尔滨: 哈尔滨工业大学, 2013.
MA X Y. Study on the Attitude Control System of Satellite with Reaction Wheels and Magnetotors [D]. Harbin: Harbin Institute of Technology, 2013.(in Chinese)
王 鑫 , 张 妍 , 尹 玉明 , 等 . 微小卫星标准化现状的分析及思考 . 中国航天 , 2018 . ( 12 ): 36 - 40 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201812009 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201812009 .
X WANG , Y ZHANG , Y M YIN , 等 . Analysis and thoughts on microsatellite standardization status . Aerospace China , 2018 . ( 12 ): 36 - 40 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201812009 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=zght201812009 .
贺 广松 , 李 新洪 , 王 谦 , 等 . 模块化航天器姿态控制系统仿真研究 . 现代电子技术 , 2018 . 41 ( 18 ): 131 - 134 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xddzjs201818030 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xddzjs201818030 .
G S HE , X H LI , Q WANG , 等 . Simulation research on Attitude Control System for Modular Spacecraft . Modern Electronics Technique , 2018 . 41 ( 18 ): 131 - 134 . http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xddzjs201818030 http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=xddzjs201818030 .
王志远.基于微型动量轮组的皮纳卫星姿态控制系统研究[D].杭州: 浙江大学, 2017.
WANG ZH Y. Research on the Attitude Control System for Nano-satellites Based on Micro-Reaction Wheels Units [D]. Hangzhou: Zhejiang University, 2017.(in Chinese)
戴 路 , 金 光 , 陈 涛 . 基于VSCMG的卫星姿态控制仿真系统 . 光学 精密工程 , 2008 . 16 ( 8 ): 1546 - 1553 . http://ope.lightpublishing.cn/thesisDetails?columnId=1745181&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1745181&Fpath=&index=-1&l=zh .
L DAI , G JIN , T CHEN . Satellite attitude control simulation test bed based on VSCMG . Opt. Precision Eng. , 2008 . 16 ( 8 ): 1546 - 1553 . http://ope.lightpublishing.cn/thesisDetails?columnId=1745181&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1745181&Fpath=&index=-1&l=zh .
徐 开 , 金 光 , 陈 娟 , 等 . 敏捷小卫星姿态机动切换算法 . 光学 精密工程 , 2008 . 16 ( 8 ): 1528 - 1532 . http://ope.lightpublishing.cn/thesisDetails?columnId=1744650&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1744650&Fpath=&index=-1&l=zh .
K XU , G JIN , J CHEN , 等 . Switch algorithm for quick small satellite attitude maneuver . Opt. Precision Eng. , 2008 . 16 ( 8 ): 1528 - 1532 . http://ope.lightpublishing.cn/thesisDetails?columnId=1744650&Fpath=&index=-1&l=zh http://ope.lightpublishing.cn/thesisDetails?columnId=1744650&Fpath=&index=-1&l=zh .
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