Research on Tether Assisted Interplanetary Orbital Capture

doi:10.3780/j.issn.1000-758X.2014.06.003

Chinese Space Science and Technology ›› 2014, Vol. 34 ›› Issue (6): 15-.doi: 10.3780/j.issn.1000-758X.2014.06.003

Previous Articles Next Articles

Research on Tether Assisted Interplanetary Orbital Capture

LIU Bin-Bin^1,2, HUANG Pan-Feng^1,2, MENG Zhong-Jie^1,2

(1 Research Center of Intelligent Robotics,School of Astronautics,Northwestern Polytechnical University,Xi'an 710072)(2 National Key Laboratory of Aerospace Flight Dynamics,Northwestern Polytechnical University,Xi'an 710072)

Received:2014-03-19 Revision received:2014-07-06 Online:2014-12-25 Published:2014-12-25

Abstract

Abstract: Tether control of the momentum exchange tether assisted interplanetary orbital capture in deep space exploration was studied. Firstly, the dynamic model of a detector system in a hyper bolic flying orbit was established. Secondly,the consistent condition of orbital capture and the optimum tether cut off point were derived to analyze the dynamic characteristics.Finally, considering the sub detectors post capture orbit maneuver requirements and limitation of the tether deployment/retrieval velocity, a new optimal control problem was proposed and numerically solved by the simulated annealing algorithm.Simulation results show that the tether orientation is appropriate at the cut off point and will be beneficial for the following orbit maneuver,and the maximum tether deployment/retrieval velocity is about 30m/s.

Key words: Deep space exploration, Momentum-exchange tether, Orbitalcapture, Capture condition, Optimal control

LIU Bin-Bin, HUANG Pan-Feng, MENG Zhong-Jie. Research on Tether Assisted Interplanetary Orbital Capture[J]. Chinese Space Science and Technology, 2014, 34(6): 15-.

Add to citation manager EndNote|Reference Manager|ProCite|BibTeX|RefWorks

URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2014.06.003

https://journal26.magtechjournal.com/kjkxjs/EN/Y2014/V34/I6/15

[1]	WANG Yujie, LI Xizhi, KONG Dali. A study on subsurface ocean property inversion of icy moons using multi-frequency magnetic induction response [J]. Chinese Space Science and Technology, 2025, 45(4): 23-36.
[2]	LIU Jianghui, PENG Qibo, WU Xinfeng. An optimal control strategy for spacecraft approaching along a designated straight direction [J]. Chinese Space Science and Technology, 2025, 45(3): 110-119.
[3]	LI Ruifeng, SUN Chong, WANG Zheng, FANG Qun, ZHANG Xiang. Capture configuration design for space non-cooperative target based on reachable domain [J]. Chinese Space Science and Technology, 2024, 44(5): 83-94.
[4]	WU Chenchen, GENG Hai, WANG Zitong, LI Detian. Development of advanced electric propulsion technology for cislunar and deep space exploration [J]. Chinese Space Science and Technology, 2023, 43(5): 13-23.
[5]	GENG Hai, LI Xingda, JIA Lianjun, JIA Yanhui, WU Chenchen, SUN Mingming, SUN Xinfeng. Life prediction of 30cm ion thruster for deep space exploration [J]. Chinese Space Science and Technology, 2022, 42(6): 107-114.
[6]	HU Hang, LIU Lei, LI Cong, CAO Gui Xing. Research on composite scanning strategy for high-probability acquisition of deep space cooperative targets [J]. Chinese Space Science and Technology, 2022, 42(3): 58-66.
[7]	MA Xin, ZHOU Qi, LI Mingtao, ZHANG Huisuo. Overall technology analysis and efficiency simulation of the deep space impactor [J]. Chinese Space Science and Technology, 2021, 41(1): 120-130.
[8]	YE Zipeng, ZHOU Qingrui, WANG Hui. Research on autonomous navigation method for deep space exploration spacecraft in cruise phase [J]. Chinese Space Science and Technology, 2020, 40(5): 53-60.
[9]	LU Wei-Tao, XIE Jian-Feng, CHEN Lue- Ren-Tian-Peng, HAN Song-Tao, WANG Mei. An interferometry method based on signal combination [J]. Chinese Space Science and Technology, 2019, 39(4): 54-.
[10]	KUAI Zhengzhong, SHEN Hongxin, LI Hengnian, HE Qingbo. Optimal station keeping of geostationary satellites by electric propulsion [J]. Chinese Space Science and Technology, 2018, 38(3): 69-75.
[11]	Yang-Hong-Wei, CHEN Yang, BAO Yin-He-Xi, LI Jun-Feng. Trajectory Design of Gravity Assist in the High-fidelity Dynamic Model [J]. Chinese Space Science and Technology, 2013, 33(2): 1-6.
[12]	MA Ke-Mao, CHEN Hai-Peng. Optimal Trajectory Design for the Lunar Module in Ascent Stage [J]. Chinese Space Science and Technology, 2013, 33(2): 54-60.
[13]	LIU Lei, LIU Yong, CAO Jian-Feng, TANG Ge-Shi, HU Song-Jie. Kinetic Characteristics and Continuation Algorithm of Periodic Families [J]. Chinese Space Science and Technology, 2013, 33(1): 30-36.
[14]	LU Wei-Tao, YANG Wen-Ge, HONG Jia-Cai, SHI Xue-Shu. FX Correlation Scheme and Improvement on Delete Algorithm [J]. Chinese Space Science and Technology, 2012, 32(6): 54-61.
[15]	HE Zhao-Wei, SHI Peng, GE Bing, ZHAO Yu-Shan. Optimal Cooperative Rendezvous of Spacecraft Considering Locations of Capture Interfaces [J]. Chinese Space Science and Technology, 2011, 31(6): 36-42.

Research on Tether Assisted Interplanetary Orbital Capture

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments