Simulation and Experiment on the Influence of Micro Vibration on Pointing Measurement of High-Performance Spacecraft

LI Lin1,2, GONG Xiaoxue3, ZHU Feihu1,2, YU Yang3,4,5, ZHAO Qin1,2, ZHANG Lei3,4, ZHANG Yunfang1,2, WU Yanpeng1,2, WANG Li1,2

PDF(927 KB)
PDF(927 KB)
Journal of Deep Space Exploration ›› 2023, Vol. 10 ›› Issue (3) : 277-282. DOI: 10.15982/j.issn.2096-9287.2023.20220056
Special Issue:Space Gravitational Wave Detection
Special Issue:Space Gravitational Wave Detection

Simulation and Experiment on the Influence of Micro Vibration on Pointing Measurement of High-Performance Spacecraft

  • LI Lin1,2, GONG Xiaoxue3, ZHU Feihu1,2, YU Yang3,4,5, ZHAO Qin1,2, ZHANG Lei3,4, ZHANG Yunfang1,2, WU Yanpeng1,2, WANG Li1,2
Author information +
History +

Abstract

The micro-vibration of ultra-high-static and ultra-high-stable spacecraft was studied. A modeling and simulation method was proposed to introduce the pointing measurement error and additional torque error induced by micro-vibration into the pointing measurement control system. The micro-vibration experiment of the pointing measurement system was carried out based on the quasi-zero stiffness suspension method. The simulation and experimental results show that the pointing measurement error induced by micro-vibration was more significant, and the peak value reached 10e-4°, and the pointing measurement error of the pointing control system caused by micro-vibration was 0.03 pixels. This work can be used for reference in the study of ultra-high-static and ultra-high-stable spacecraft and derivative technologies.

Keywords

micro vibration / high performance spacecraft / pointing measurement error / closed-loop modeling method

Cite this article

Download citation ▾
LI Lin, GONG Xiaoxue, ZHU Feihu, YU Yang, ZHAO Qin, ZHANG Lei, ZHANG Yunfang, WU Yanpeng, WANG Li. Simulation and Experiment on the Influence of Micro Vibration on Pointing Measurement of High-Performance Spacecraft. Journal of Deep Space Exploration, 2023, 10(3): 277‒282 https://doi.org/10.15982/j.issn.2096-9287.2023.20220056

References

[1] JULIA S,WU C L. The role for regional anesthesia in medical emergencies during deep space flight[J]. Regional anesthesia and pain medicine,2021,46(10):919-922
[2] KUMAR A,KRISHNAN P. Performance analysis of radio-over-free-space optical communication system with spatial diversity over combined channel model[J]. Optical and Quantum Electronics,2022,54(4):1-14
[3] SANNIBALE V,ORTIZ G G,FARR W H. A sub-hertz vibration isolation platform for a deep space optical communication transceiver[J]. Proc Spie,2009,7199:1-8
[4] BRUGAROLAS P,ALEXANDER J,TRAUGER J,et al. ACCESS pointing control system[J]. Proc Spie,2010,7731(1):77314V-77314V-22
[5] PLATE M T,O’SULLIVAN B,FERRUIT P,et al. The European optical contribution to the James Webb Space Telescope[J]. Advanced Optical Technologies,2018,7(6):353-364
[6] 李林,袁利,王立,等. 从哈勃太空望远镜剖析微振动对高性能航天器指向测量与控制系统的影响[J]. 光学精密工程,2020,28(11):2478-2487
LI L,YUAN L,WANG L,et al. Influence of micro vibration on measurement and pointing control system of high-performance spacecraft from Hubble Space Telescope[J]. Optics and Precision Engineering,2020,28(11):2478-2487
[7] HAMMESDAHR A. LISA mission study overview[J]. Class Quantum Grav,2001,18:4045-4051
[8] HU W R,WU Y L. The Taiji program in space for gravitational wave physics and the nature of gravity[J]. Natl Sci Rev,2017(4):685-686
[9] LUO J,CHEN L S,DUAN H Z,et al. TianQin:a spaceborne gravitational wave detector[J]. Classical and Quantum Gravity,2016,33(3):035010
[10] 张立华,黎明,高永新,等. 空间引力波探测航天器系统及平台技术[J]. 中山大学学报:自然科学版,2021,60(1-2):129-137
ZHANG L H,LI M,GAO Y X,et al. The spacecraft system and platform technologies for gravitational wave detection in space[J]. Acta Scientiarum Naturalium Universitatis Sunyatseni,2021,60(1-2):129-137
[11] EYERMAN C E. A system engineering approach to disturbance minimization for spacecraft utilizing controlled structures technology [D]. Massachusetts:Massachusetts Institute of Technology ,1990.
[12] LANGE B. The control anduse of drag free satellites[D]. Stanford California:Stanford University,1964.
[13] 傅江良,甘庆波,张 扬,等. 无拖曳航天任务检验质量的设计和比较[J]. 中国光学,2019,12(3):463-476
FU J L,CAO Q B,ZHANG Y,et al. Design and trade-off study of proof masses for future spatial drag-free missions[J]. Chinese Optics,2019,12(3):463-476
[14] 邓剑峰,蔡志鸣,陈 琨,等. 无拖曳控制技术研究及在我国空间引力波探测中的应用[J]. 中国光学,2019,12(3):503-514.
DENG JF,CAI ZM,CHEN K,et al Drag-free control and its application in China’s spae gravitational wave detection[J]. Chinese Optics,2019,12(3):463-476.
[15] LI L,YUAN L,WANG L,et al. Recent advances in precision measurement & pointing control of spacecraft[J]. Chinese Journal of Aeronautics,2021,34(10):191-209
[16] AMBERG V,DECHOZ C,BERNARD L,et al. In-flight attitude perturbances estimation:application to PLEIADES-HR satellites[J]. Proc Spie,2013,8866:886612
[17] LI L,WANG L,YUAN L,et al. Micro-vibration suppression methods and key technologies for high-precision space optical instruments[J]. Acta Astronautica,2020,180(4):417-428
[18] PEDREIRO N,BETHESDA M D. Spacecraft architecture for disturbance-free payloa:USA,US-6454215-B1[P]. 2002.
[19] NELSON P. Spacecraft architecture for disturbance-free payload:USA,US 09/770252 [P]. 2001-01-29.
[20] PEDREIRO N,CARRIER A,LORELL K,et al. Disturbance-free payload concept demonstration[C]//AIAA guidance,navigation,& control conference & exhibit. Monterey,USA:AIAA,2002.
[21] MICHAEL A. GONZALES,NELSON P,et al. Unprecedented vibration isolation demonstration using the disturbance-free payload concept[C]//Proceedings of AIAA guidance,navigation,and control conference and exhibit. Rhode Island:AIAA,2004.
[22] 杨鸿杰,刘磊,李新国,等. 超静超稳卫星碰振动力学建模[J]. 宇航学报,2019,40(8):861-869
YANG H J,LIU L,LI XG,et al. Vibro-impact Modeling for Disturbance-Free Payload Satellite[J]. Journal of Astronautics,2019,40(8):861-869
[23] 张伟,赵艳彬,廖鹤,等. 动静隔离、主从协同控制双超卫星平台设计[J]. 上海航天,2014,31(5):7-11,30
ZHANG W,ZHAO Y B,LIAO H,et al. Design of an active-quiet isolated and master-slave coordination controlled dual-super satellite platform[J]. Aerospace Shanghai,2014,31(5):7-11,30
[24] 汤亮,王有懿,关新,等. 一种超精超稳超敏捷控制在轨验证方法:中国,CN108762231A[P]. 2018-11-06.
[25] YUAN L,WANG M M,WU Y P,et al. Review on development of space starlight measurement technology[J]. Acta Aeronaut Astronaut Sinica,2020,41(8):7-18+2
[26] ARONSTEIN D L,SMITH J S,ZIELINSKI T P,et al. Wavefront-error performance characterization for the James Webb Space Telescope (JWST) Integrated Science Instrument Module (ISIM) science instruments[C]//Proceedings of SPIE Astronomical Telescopes & Instrumentation. Edinburgh,United Kingdom:SPIE,2016.
[27] LI M,ZHANG Y,WANG Y,et al. The pointing and vibration isolation integrated control method for optical payload[J]. Journal of Sound and Vibration,2019,438:441-456
[28] FENG Z,CUI Y,YANG X ,et al. Micro-vibration issues in integrated design of high resolution optical remote sensing satellites. Proceedings in Physics[C]//Proceedings of 3rd International Symposium of Space Optical Instruments and Applications. Beijing,China:Springer,2017.
[29] LI L,TAN L Y,KONG L,et al. The influence of flywheel micro-vibration on space camera and vibration sup-pression[J]. Mechanical Systems and Signal Processing,2018,100:360-370
[30] LI L,YUAN L,WANG L,et al. Image motion and experimental study of a 0.1″ space pointing measuring instrument for micro-vibration conditions[J]. Chinese Journal of Aeronautics,2022,36(2): 1-10.
[31] GONG X,LI L,YU Y,et al. Error analysis and calibration of micro-vibration test platform developed for advanced pointing instrument[J]. Mechanical Systems and Signal Processing,2022,173:109055
PDF(927 KB)

Accesses

Citations

Detail

Sections
Recommended

/