Trajectory Optimization Design for Multiple-Target Asteroid Flyby Mission in Ecliptic Plane

HAO Zhixin1,2, ZHENG Jianhua1,2, LI Mingtao1,2

PDF(1101 KB)
PDF(1101 KB)
Journal of Deep Space Exploration ›› 2022, Vol. 9 ›› Issue (4) : 373-381. DOI: 10.15982/j.issn.2096-9287.2022.20210143
Special Issue: Small Celestial Body Exploration and Defense
Special Issue: Small Celestial Body Exploration and Defense

Trajectory Optimization Design for Multiple-Target Asteroid Flyby Mission in Ecliptic Plane

  • HAO Zhixin1,2, ZHENG Jianhua1,2, LI Mingtao1,2
Author information +
History +

Abstract

Closely flying by asteroids can help to capture asteroid surface images,measure asteroid spectra,and obtain physical and chemical properties of asteroids. In particular,flying by multiple asteroids with potential hazards to the earth in one mission will significantly improve the understanding of the characteristics of potentially hazardous asteroids,and it is also of great significance to asteroid defense missions. In this paper,the trajectory of the multiple asteroid flyby mission of potentially hazardous asteroids was optimized. Firstly,the time and position distribution of asteroids passing through the ecliptic plane were analyzed,and the basic strategy of asteroids flyby in the ecliptic was determined. The time of asteroids crossing the ecliptic was taken as the time of asteroids’ flyby. Secondly,the sequential flyby sequence was optimized via beam selection tree search algorithm,and an optimization model for fast and effective solution of asteroid sequential flyby mission trajectory was established. Simulation results show that missions launched from 2024 to 2028 can fly by at least 18 potentially hazardous asteroids,especially the launch window in September 2027,which can fly by 21 potentially hazardous asteroids within a ten-year mission duration.

Keywords

potentially hazardous asteroids / multiple-target asteroid flyby / trajectory optimization / beam search

Cite this article

Download citation ▾
HAO Zhixin, ZHENG Jianhua, LI Mingtao. Trajectory Optimization Design for Multiple-Target Asteroid Flyby Mission in Ecliptic Plane. Journal of Deep Space Exploration, 2022, 9(4): 373‒381 https://doi.org/10.15982/j.issn.2096-9287.2022.20210143

References

[1] SCHULTE P,ALEGRET L,ARENILLAS I,et al. The chicxulub asteroid impact and mass extinction at the cretaceous-paleogene boundary[J]. Science,2010,327(5970):1214-1218
[2] 龚自正,李明,陈川,等. 小行星监测预警、安全防御和资源利用的前沿科学问题及关键技术[J]. 科学通报,2020,65(5):346-372
GONG Z Z,LI M,CHENG C,et al. The frontier science and key technologies of asteroid monitoring and early warning,security defense and resource utilization[J]. Chinese Science Bulletin,2020,65(5):346-372
[3] 廖慧兮,王彤,贾晓宇. 小行星探测进展及技术特点分析[J]. 国际太空,2017(7):2-9
[4] VETRISANO M,VASILE M. Autonomous navigation of a spacecraft formation in the proximity of an asteroid[J]. Advance in Space Research,2016,57(8):1783-1804
[5] WALKER L,CARLO D M,GRECO C,et al. A mission concept for the low-cost large-scale exploration and characterisation of near Earth objects[J]. Advances in Space Research,2020,67(11):3880-3908
[6] SMPAG. SMPAG statement of support for small-class,high-velocity flyby missions to small bodies for planetary defence[EB/OL]. (2021-03-25). https://www.cosmos.esa.int/web/smpag/meeting-16-mar-2021-.
[7] WATANABE S I,TSUDA Y,YOSHIKAWA M,et al. Hayabusa2 Mission Overview[J]. Space Science Reviews,2017,208(1-4):3-16
[8] RUSSELL T C,CAPACCIONI F,CORADINI A,et al. Dawn mission to Vesta and Ceres[J]. Earth,Moon,and Planets,2007,101(1-2):65-91
[9] MARCHI S,OLKIN C B. Lucy in the sky with Trojan asteroids[J]. Nature Astronomy,2021,5(11):1178-1178
[10] SARLI B V,HORIKAWA M,YAM C H,et al. DESTINY+ trajectory design to(3200)Phaethon[J]. The Journal of the Astronautical Sciences,2018,65(1):82-110
[11] GATER W. Comet mission given green light by European Space Agency[J]. Physics World,2019,32(8):13
[12] GAO Y,LU X,PENG Y,et al. Trajectory optimization of multiple asteroids exploration with asteroid 2010TK7 as main target[J]. Advances in Space Research,2019,63(1):432-442
[13] 夏炎,罗永杰,赵海斌,等. 主带小行星深空探测可接近性与多目标探测轨道的实现[J]. 天文学报,2010,51(2):163-172
XIA Y,LUO Y J,ZHAO H B,et al. Accessibility for main belt asteroid exploration and trajectory design for multiple asteroids[J]. Acta Astronomica Sinica,2010,51(2):163-172
[14] QIAO D,CUI P Y,CUI H H. Proposal for a multiple-asteroid-flyby mission with sample return[J]. Advances in Space Research,2012,50(3):327-333
[15] MCNUTT L,JOHNSON L,CLARDY D,et al. Near-earth asteroid(NEA)scout[C]//AIAA Space 2014 Conference and Exposition. San Diego,CA:AIAA,2014.
[16] GRECO C,DI CARLO M,WALKER L,et al. Analysis of NEOs reachability with nano-satallites and low-thrust propulsion[C]//4S Symposium 2018-Small Satellites Systems and Services. [S. l. ]:AIAA,2018.
[17] CATALDI G,MARCUCCIO S. A 2-D Trajectory design algorithm for multiple asteroid flyby missions[J]. Aerotecnica Missili & Spazio,2020,99(4):287-295
[18] LI S,HUANG X Y,YANG B. Review of optimization methodologies in global and China trajectory optimization competitions[J]. Progress in Aerospace Sciences,2018,102:60-75
[19] SHIRAZI A,CEBERIO J,LOZANO J A. Spacecraft trajectory optimization:a review of models,objectives,approaches and solutions[J]. Progress in Aerospace Sciences,2018,102:76-98
[20] JIANG F,CHEN Y,LIU Y,et al. GTOC5:results from the Tsinghua University[J]. Acta Futura,2014,8(1):37-44
[21] IZZO D,HENNES D,SIMÕES L F,et al. Designing complex interplanetary trajectories for the global trajectory optimization competitions[M]. Switzerland:Springer,Cham,2016.
[22] LUO Y,ZHU Y,ZHU H,et al,GTOC9:results from the national university of defense technology[J]. Acta Futura,2018(11):37-47.
[23] CASALINO L,PASTRONE D,SIMEONI F,et al. GTOC5:results from the Politecnico di Torino and Università di Roma Sapienza[J]. Acta Futura,2014,8(1):29-36
[24] PETROPOULOS A E,BONFIGLIO E P,GREBOW D J,et al. GTOC5:results from the Jet Propulsion Laboratory[J]. Acta Futura,2014,8(1):21-27
[25] HD· 柯蒂斯 (美). 轨道力学[M]. 周建华,徐波,冯全胜,译. 北京:科学出版社,2009.
[26] LI H Y,BAOYIN H X. Sequence optimization for multiple asteroids rendezvous via cluster analysis and probability-based beam search[J]. Science China Technological Sciences,2021,64(1):122-130
[27] ESA. Near-Earth objects coordination centre [EB/OL]. [2021-11-20]. https://neo.ssa.esa.int/search-for-asteroids.
[28] LIU J,ZHENG J,LI M. Dry mass optimization for the impulsive transfer trajectory of a near-Earth asteroid sample return mission[J]. Astrophysics and Space Science,2019,364(12):1-14
[29] SHEN H X,ZHANG T J,HUANG A Y,et al. GTOC9:results from the Xi’an Satellite Control Center(team XSCC)[J]. Acta Futura,2018,11:49-55
PDF(1101 KB)

Accesses

Citations

Detail

Sections
Recommended

/