Natural formation of a nano/micro spacecraft cluster for multi-model distributed remote sensing

FANG Yuankun; MENG Ziyang; YOU Zheng

doi:10.16511/j.cnki.qhdxxb.2018.25.021

PDF(1421 KB)

Journal of Tsinghua University(Science and Technology) ›› 2018, Vol. 58 ›› Issue (5) : 482-488. DOI: 10.16511/j.cnki.qhdxxb.2018.25.021

PRECISION INSTRUMENT

Natural formation of a nano/micro spacecraft cluster for multi-model distributed remote sensing

{{article.zuoZhe_EN}}

Author information +

History +

Abstract

Distributed remote sensing has attracted much attention for space exploration. The sensing ability is based on the system properties of the spacecraft cluster composed by multiple nano/micro spacecraft. In addition, the multiple nano/micro spacecraft formation can be rearranged for different applications. However, since the micro/nano spacecraft have little fuel, methods are urgently needed to maintain the stability of the distributed remote sensing nano/micro spacecraft formation for a relatively long period in a natural formation.The natural nano/micro spacecraft cluster formation is analyzed have for a multiple distributed remote sensing task scenario that optimizes the fuel usage and calculational efficiency. A direct parameter method was designed for the typical tasks of in-plane flying with a tree communication topology and leader-following topology modes. The orbit parameters of the followers are obtained directly by this method. STK simulations show this approach is accurate, robust, and useful for emergency remote sensing tasks.

Key words

distributed remote sensing / formation of nano/micro spacecraft / natural formation

Cite this article

EndNote

Ris (Procite)

Bibtex

Download Citations

FANG Yuankun, MENG Ziyang, YOU Zheng. Natural formation of a nano/micro spacecraft cluster for multi-model distributed remote sensing[J]. Journal of Tsinghua University(Science and Technology). 2018, 58(5): 482-488 https://doi.org/10.16511/j.cnki.qhdxxb.2018.25.021

References

[1] 周美江, 吴会英, 齐金玲.微纳卫星共面伴飞相对运动椭圆短半轴最省燃料控制[J]. 中国空间科学技术, 2015, 5(4):22-31.ZHOU M J, WU H Y, QI J L. Minimum fuel control of the elliptic short axis of the relative motion in micro/nano satellite coplanar flying[J]. Chinese Space Science and Technology, 2015, 5(4):22-31. (in Chinese)
[2] 张育林, 曾国强, 王兆魁, 等. 分布式卫星系统理论及应用[M]. 北京:科学出版社, 2008.ZHANG Y L, ZENG G Q, WANG Z K. Theory and application of distributed satellite system[M]. Beijing:Science Press, 2008. (in Chinese)
[3] SABOL C, BUMS R, MCLAUGHLIN C A. Satellite formation flying design and evolution[J]. Journal of Spacecraft and Rocket, 2001, 38(2):270-278.
[4] CARTER T E. New form for the optimal rendezvous equations near a Keplerian orbit[J]. Journal of Guidance, Control, and Dynamics, 1990, 13(1):183-186.
[5] SCHWEIGHART S A, SEDWICK R J. High fidelity linearized J₂ model for satellite formation flight[J]. Journal of Guidance, Control, and Dynamics, 2002, 25(6):1073-1080.
[6] VADALI S R, ALFRIEND K T, VADDI S. Hill's equations, mean orbital elements, and formation flying of satellites[C]//The Richard H. Battin Astrodynamics Symposium. College Station, TX, USA:AAS, 2000:187-203.
[7] AFFRIEND K T, SCHANB H, GIM D W. Gravitational perturbations, nonlinearity and circular orbit assumption effects on formation flying control strategies[C]//AAS Guidance and Control Conference. San Diego, CA, USA:AAS, 2000:1-12.
[8] SCHAUB H, ALFRIEND K T. J₂ invariant relative orbits for spacecraft formations[J]. Celestial Mechanics and Dynamical Astronomy, 2001, 79(2):77-95.
[9] 孟云鹤. 航天器编队飞行导论[M]. 北京:国防工业出版社, 2014.MENG Y H. Introduction to spacecraft formation flying[M]. Beijing:National Defend Industry Press, 2014. (in Chinese)
[10] 吴宝林, 曹喜滨, 任子武. 一种长期稳定的卫星编队队形优化设计方法[J]. 航空学报, 2007, 28(1):167-172.WU B L, CAO X B, REN Z W. A long-time stable formation optimal design method for satellite formation[J]. Acta Aeronautica Astronautica Sinica, 2007, 28(1):167-172. (in Chinese)
[11] 刘林.航天器轨道理论[M]. 北京:国防工业出版社, 2000.LIU L. Orbit theory of spacecraft[M]. Beijing:National Defend Industry Press, 2000. (in Chinese)
[12] 孟鑫, 李俊峰, 高云峰. 编队飞行卫星相对运动的零J₂摄动条件[J]. 清华大学学报(自然科学版), 2004, 44(2):219-223. MENG X, LI J F, GAO Y F. J₂ invariant perturbation conditions for the relative movement for satellites in formation flying[J]. Journal of Tsinghua University (Science and Technology), 2004, 44(2):219-223. (in Chinese)