Optimal Cooperative Rendezvous of Spacecraft Considering Locations of Capture Interfaces

doi:10.3780/j.issn.1000-758X.2011.06.006

›› 2011, Vol. 31 ›› Issue (6): 36-42.doi: 10.3780/j.issn.1000-758X.2011.06.006

Previous Articles Next Articles

Optimal Cooperative Rendezvous of Spacecraft Considering Locations of Capture Interfaces

HE Zhao-Wei, SHI Peng, GE Bing, ZHAO Yu-Shan

(School of Astronautics, Beihang University, Beijing 100191)

Received:2011-03-02 Revised:2011-12-25 Published:2011-12-25 Online:2011-12-25

Abstract

Abstract: The optimal close range rendezvous of two spacecrafts was investigated. The complete 26 state model with six degree of freedom for the rendezvouswas developed to prevent the undesired collision of spacecraft considering the attitude change, the locations of capture interfaces, and the pathconstraints. The minimum quadratic control and minimum time problems were discretized into the problem of large scale onlinear programming bymeans of Gaussian pseudospectral method, which was solved by the software package SNOPT. The influences of different initial parameters on theoptimal solutions were also analyzed. Numerical simulation results show that the time and fuel cost may be decreased with the optimal cooperativerendezvous compared with the optimal active passive rendezvous.

Key words: Cooperative rendezvous, Optimal control, Gaussian pseudospectral method, Spacecraft

HE Zhao-Wei, SHI Peng, GE Bing, ZHAO Yu-Shan. Optimal Cooperative Rendezvous of Spacecraft Considering Locations of Capture Interfaces[J]. , 2011, 31(6): 36-42.

0
/ / Recommend

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

URL: http://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2011.06.006

http://journal26.magtechjournal.com/kjkxjs/EN/Y2011/V31/I6/36

[1]	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.
[2]	LIUWei,CHENLiping,DINGJianwan,XIEGang. ModelingandAnalysisofCabinAtmosphericEnvironmentalControlSysteminaMannedSpacecraft [J]. , 2015, 35(3): 50-.
[3]	WEN Wen, ZONG Guang-Hua, YU Yang, SUN Liang. Research on Denoising Method for Small PipeUltrasonic Flow Meter [J]. , 2015, 35(2): 77-.
[4]	LIU Bin-Bin, HUANG Pan-Feng, MENG Zhong-Jie. Research on Tether Assisted Interplanetary Orbital Capture [J]. , 2014, 34(6): 15-.
[5]	MA Ke-Mao, CHEN Hai-Peng. Optimal Trajectory Design for the Lunar Module in Ascent Stage [J]. , 2013, 33(2): 54-60.
[6]	GAO Peng, LUO Jian-Jun. Adaptive Artificial Potential Function Guidance for Dynamic Obstacle Avoidance of Spacecraft [J]. , 2012, 32(5): 1-8.
[7]	TIAN Lin, XU Shi-Jie. Adaptive Attitude Control of Spacecraft with Variable Speed Control Moment Gyroscopes [J]. , 2012, 32(5): 9-16.
[8]	ZHANG Tao-Tao, BAI Xian-Zong, HAO Jia, CHEN Lei. LEOSpacecraftOrbitAnomalyDetectionBasedonPredictionDispersion [J]. , 2012, 32(5): 40-46.
[9]	SHEN Zi-Cai, QIU Jia-Wen, DING Yi-Gang, LIU Yu-Ming, ZHAO Chun-Qing. SpaceEnvironmentSynergisticEffectonSpacecraft [J]. , 2012, 32(5): 54-60.
[10]	CHENG Xing, SHI Xiao-Ning, CUI Nai-Gang. Inverse Polynomial Shape based Method for Low thrust Trajectory Design [J]. , 2011, 31(6): 1-7.
[11]	Jin Lei Xu Shijie (School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191). Attitude Stabilization of an Underactuated Spacecraft with Two Reaction Wheels [J]. , 2009, 29(02): 8-16.
[12]	Lu ShanXu Shijie(School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100083). Optimal Control Method for Satellite Formation in Elliptical Orbit [J]. , 2008, 28(01): 18-26.
[13]	Wang Mingguang Pei Tingguo(The Academy of China Aerospace Times Electronic Corporation,Beijing 100070)Yuan Jianping(College of Astronautics,Northwestern Polytechnical University,Xi'an 710072). Legendre Pseudospectral Method for Rapid Lunar Soft-Landing Trajectory Optimization [J]. , 2007, 27(05): 27-32.
[14]	Wu Delong Peng Weibin (Beijing Institute of Astronautical Systems Engineering, Beijing 100076). Optimal Aeroassisted Orbital Interception and Rendezvous [J]. , 2004, 24(02): -.
[15]	Wang Hua Tang Guojin Lei Yongjun (College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073). The Direct Shooting Method Solving Finite-Thrust Trajectory Optimization [J]. , 2003, 23(05): -.

Optimal Cooperative Rendezvous of Spacecraft Considering Locations of Capture Interfaces

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments