空间用四轴陀螺组合浪涌防护及数据填补方法

doi:10.12305/j.issn.1001-506X.2021.12.28

Abstract

Abstract:

Aiming at the problems of surge and data loss when the four-axis gyro combination is used for space axial switching and light source switching, a surge protection and data filling method is proposed. Firstly, the dual light source scheme is adopted, and the surge protection circuit is designed to reduce the impact of the instantaneous high current on the components during the power-on process. Secondly, a data filling mechanism is established to compensate for the data lost during the switching process. Finally, the ground data filling experiment is carried out, the angular rate is set to 0.174 5 rad/s and 1.745 rad/s, the difference between the predicted angular rate and the actual angular rate are no more than 0.003 rad/s and 0.008 rad/s, and the relative residuals are 0.003 9 and 0.001 2 respectively, which verifying the effectiveness of the proposed method.

Key words: space application, redundant design, surge protection, grey forecast

CLC Number:

TN927

Minpeng DAI, Chunxi ZHANG, Yanqiang YANG. Spatial four-axis gyro combination surge protection and data filling method[J]. Systems Engineering and Electronics, 2021, 43(12): 3652-3657.

Figures/Tables 6

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References 30

1	程一凡, 曲至诚, 张更新. 低轨卫星星座物联网业务量建模[J]. 电子与信息学报, 2021, 43 (4): 1050- 1056.
	CHENG Y F , QU Z C , ZHANG G X . Traffic modeling for low earth orbit satellite constellation internet of things[J]. Journal of Electronics and Information Technology, 2021, 43 (4): 1050- 1056.
2	王磊, 李德仁, 陈锐志, 等. 低轨卫星导航增强技术—机遇与挑战[J]. 中国工程科学, 2020, 22 (2): 144- 152.
	WANG L , LI D R , CHEN R Z , et al. Low earth orbiter (LEO) navigation augmentation: opportunities and challenges[J]. Strategic Study of Chinese Academy of Engineering, 2020, 22 (2): 144- 152.
3	MARSIS J , NAHIMANA D F , VIANDIER N , et al. GNSS accuracy enhancement based on pseudo range error estimation in an urban propagation environment[J]. Expert Systems with Applications, 2013, 40 (15): 5956- 5964. doi: 10.1016/j.eswa.2013.05.026
4	ZHENG S Y , LI R , HUANG Z G , et al. Determination of fast corrections for satellite-based augmentation system: a user equivalent range error-based method[J]. IEEE Access, 2019, 7, 178662- 178674. doi: 10.1109/ACCESS.2019.2953096
5	MUHAMMAD A A , LIU P L , WANG Y Z , et al. GNSS position-ing accuracy enhancement based on robust statistical MM estimation theory for ground vehicles in challenging environments[J]. Applied Sciences, 2018, 8 (6): 876. doi: 10.3390/app8060876
6	张小红, 马福建. 低轨导航增强GNSS发展综述[J]. 测绘学报, 2019, 48 (9): 1073- 1087.
	ZHANG X H , MA F J . Review of the development of LEO navi gation-augmented GNSS[J]. Acta Geodaetica et Cartographica Sinica, 2019, 48 (9): 1073- 1087.
7	章燕申, 张春熹, 蒋军彪, 等. 光电子学与光学陀螺仪[M]. 北京: 清华大学出版社, 2017.
	ZHANG Y S , ZHANG C X , JIANG J B , et al. Optoelectronics and optical gyroscopes[M]. Beijing: Tsinghua University Press, 2017.
8	WANG M S , WU W Q , HE X F , et al. Consistent ST-EKF for long distance land vehicle navigation based on SINS/OD integration[J]. IEEE Trans.on Vehicular Technology, 2019, 68 (11): 10525- 10534. doi: 10.1109/TVT.2019.2939679
9	MITANI S, MIZUTANI T, SAKAI S I. Current status of fiber optic gyro efforts for space applications in Japan[C]//Proc. of the Fiber Optic Sensors & Applications XⅢ, 2016: 985208.
10	Tamagawa Seiki Company Limited. 3-axis FOG for subminiature satellite data manual[EB/OL]. [2021-02-25]. https://www.tamagawa-seiki.co.jp/products/gyro/3-axis-gyro-TA7584.html.
11	Optolink Company Limited. Single axis fiber-optic gyroscope SRS200 data manual[EB/OL]. [2021-02-25]. http://www.optolink.ru/en/products/single_axis_fog/srs-200.
12	Optolink Company Limited. Three axis fiber-optic gyroscope TRS500 data manual[EB/OL]. [2021-02-25]. http://www.optolink.ru/en/products/three_axis_fog/trs500.
13	张现亮, 朱敏波, 李琴. 空间辐照机理与防护技术研究[J]. 空间电子技术, 2007, 4 (3): 17- 20.
	ZHANG X L , ZHU M B , LI Q . Research on space irradiation mechanism and protection technology[J]. Space Electronic Technology, 2007, 4 (3): 17- 20.
14	ZHANG C X , DAI M P , PAN X , et al. High precision tri-axial quartz flexible accelerometers resolution measurement method based on tri-axial turntable[J]. IEEE Access, 2020, 8, 53463- 53470. doi: 10.1109/ACCESS.2020.2979757
15	唐圣金, 郭晓松, 王振业, 等. 基于故障树的多光纤陀螺冗余系统可靠性分析[J]. 中国惯性技术学报, 2013, 21 (2): 259- 263. doi: 10.3969/j.issn.1005-6734.2013.02.026
	TANG S J , GUO X S , WANG Z Y , et al. Reliability analysis for redundant system with multiple FOGs based on fault tree analysis method[J]. Journal of Chinese Inertial Technology, 2013, 21 (2): 259- 263. doi: 10.3969/j.issn.1005-6734.2013.02.026
16	赵琳, 苏中华, 郝勇, 等. 基于对偶数和改进EKF的敏捷卫星姿态确定算法[J]. 系统工程与电子技术, 2013, 35 (12): 2552- 2558. doi: 10.3969/j.issn.1001-506X.2013.12.18
	ZHAO L , SU Z H , HAO Y , et al. Algorithm for agile satellite attitude estimation based on dual quaternion and improved EKF[J]. Systems Engineering and Electronics, 2013, 35 (12): 2552- 2558. doi: 10.3969/j.issn.1001-506X.2013.12.18
17	MA K , SONG N F , JING J , et al. Configuration optimization in miniature interferometric fiber-optic gyroscopes for space application[J]. IEEE Sensors Journal, 2020, 20 (13): 7107- 7117. doi: 10.1109/JSEN.2020.2977584
18	JING J , XU H J , MA D Y , et al. A novel interferometric fiber optic gyroscope with random walk fault diagnosis for space application[J]. Optics and Lasers in Engineering, 2012, 50 (7): 958- 963. doi: 10.1016/j.optlaseng.2012.02.003
19	ZHU M D , SONG N F , PAN X . Research on fault diagnosis criterion for system clock of fiber optic gyroscope[J]. Optik, 2013, 124 (20): 4642- 4646. doi: 10.1016/j.ijleo.2013.01.072
20	JING J , ZHANG T , MA K , et al. Fault diagnosis of space-borne fiber optic gyros based on random walk coefficient prediction and in-orbit calculation[J]. IEEE Sensors Journal, 2017, 17 (20): 6637- 6645.
21	ZHANG H J , WANG Y T , WANG S T , et al. Prediction analysis of electromagnetic interference based on gray prediction theory[J]. Applied Mechanics & Materials, 2011, 44-47, 3731- 3735.
22	ZHANG L , XIONG Z , LIU J Y , et al. Research on virtual gyro configuration of redundant MEMS system based on ANFIS[J]. Optik, 2018, 157, 25- 30. doi: 10.1016/j.ijleo.2017.08.060
23	KORKISHKO Y N, FEDOROV V A, PRILUTSKIY V E, et al. Fiber optic gyro for space applications. Results of R&D and flight tests[C]//Proc. of the IEEE International Symposium on Inertial Sensors and Systems, 2016: 37-41.
24	LEFEVRE H, STEIB A, CLAIRE A, et al. The fiber optic gyro "adventure" at photonetics, iXsea and now iXblue[C]//Proc. of the Conference on Optical Waveguide and Laser Sensors, 2020: 57-59.
25	LU J Z , HU M Q , YANG Y Q , et al. On-orbit calibration method for redundant IMU based on satellite navigation & star sensor information fusion[J]. IEEE Sensors Journal, 2020, 20 (9): 4530- 4543. doi: 10.1109/JSEN.2020.2965136
26	El-SHEIMY N , HOU H Y , NIU X J . Analysis and modeling of inertial sensors using allan variance[J]. IEEE Trans.on Instrumentation and Measurement, 2008, 57 (1): 140- 149. doi: 10.1109/TIM.2007.908635
27	FABIAN C , ANDREW C , LENE B O . Quantifying noise in optical tweezers by allan variance[J]. Optic Express, 2009, 17 (15): 13255- 13269. doi: 10.1364/OE.17.013255
28	LESAGE P , AYI T . Characterization of frequency stability: analysis of the modified allan variance and properties of its estimate[J]. IEEE Trans.on Instrumentation and Measurement, 1984, 33 (4): 332- 336. doi: 10.1109/TIM.1984.4315235
29	LI J L , FANG J C . Not fully overlapping allan variance and total variance for inertial sensor stochastic error analysis[J]. IEEE Trans.on Instrumentation and Measurement, 2013, 62 (10): 2659- 2672. doi: 10.1109/TIM.2013.2258769
30	GJB2426A. 光纤陀螺仪测试方法[S]. 北京: 国防科学技术工业委员会, 2004.
	GJB2426A. Test methods for fiber optic gyroscope[S]. Beijing: Commission of Science, Technology and Industry for National Defence, 2004.

序号	项目	技术指标
1	零偏稳定性/((°)/h)	0.3
2	零偏重复性/((°)/h)	0.2
3	随机游走系数/((°)/$\sqrt {\rm{h}} $)	0.02
4	阈值/((°)/h)	0.4
5	标度因数非线性度/ppm	60
6	标度因数重复性/ppm	60
7	重量/g	990
8	功耗/W	8.9

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Spatial four-axis gyro combination surge protection and data filling method

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