Study on moment dumpling of electric propulsion satellite

doi:10.3780/j.issn.1000-758X.2016.0013

Chinese Space Science and Technology ›› 2016, Vol. 36 ›› Issue (1): 70-76.doi: 10.3780/j.issn.1000-758X.2016.0013

Previous Articles Next Articles

Study on moment dumpling of electric propulsion satellite

MA Xue^1,2,*， HAN Dong^1,2，TANG Liang^1,2

1Beijing Institute of Control Engineering, Beijing 100190,China
2Science and Technology on Space Intelligent Control Laboratory, Beijing 100190,China

Received:2015-11-12 Revised:2015-12-23 Published:2016-02-25 Online:2016-02-24

Abstract

Abstract: Moment dumpling of electric propulsion satellite can be established by pointing the thrust vectors slightly away from the center of mass. On the basis of this method, electric propulsion moment dumpling for both normal mode and failure mode was investigated. The analytic solution of optimal dumpling directions was given,and the question that whether the control arc should be considered was discussed. The simulation results show that proposed method can effectively perform the moment dumpling by electric thrusters.

Key words: electric propulsion, moment dumpling, low thrust control, parameter optimization, station keeping control

MA Xue, HAN Dong, TANG Liang. Study on moment dumpling of electric propulsion satellite[J]. Chinese Space Science and Technology, 2016, 36(1): 70-76.

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

URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2016.0013

https://journal26.magtechjournal.com/kjkxjs/EN/Y2016/V36/I1/70

[1]	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.
[2]	XIN Zhiping, GU Zhiru, WANG Chao, JIANG Yuanda, HU Jiusong. Digital design of power processing unit for ion electric propulsion system [J]. Chinese Space Science and Technology, 2023, 43(3): 73-80.
[3]	LIU Qi, MAO Wei, HU Peng, WEI Yanming, HU Yanlin, LI Yong, BIAN Bingxiu, LIU Xuhui. Application and development of high-precision Hall electric propulsion technology [J]. Chinese Space Science and Technology, 2023, 43(2): 1-15.
[4]	ZHANG Yuanzhe, HAN Xianwei, YANG Zhenyu, LU Haifeng, TAN Chang. Ion beam characteristics of iodine RF ion thruster optical system [J]. Chinese Space Science and Technology, 2022, 42(6): 115-124.
[5]	ZHANG Lupeng, YANG Xin, CHANG Lei, XU Qian, ZHOU Haishan, LUO Guangnan. Research of thrust measurement for space electric propulsion [J]. Chinese Space Science and Technology, 2022, 42(3): 25-38.
[6]	WANG Jue, WANG Min, GUO Tingting, ZHONG Xiaoqing, WEN Zheng, WEI Xin. Feasibility study of spacecraft gravity center offset compensation by intentional xenon temperature control [J]. Chinese Space Science and Technology, 2022, 42(2): 39-45.
[7]	LIU Hui, WANG Shangsheng, YU Daren, ZHAO Mingxuan, ZHENG Siyuan, CHEN Ye. Newton electric propulsion system for space gravitational wave detection [J]. Chinese Space Science and Technology, 2021, 41(5): 10-20.
[8]	CHEN Xinwei, GU Zuo, GAO Jun, GUO Ning, WANG Shangmin, ZHAO Yong, FENG Jie, SHI Kai, PU Yangxu, LI He. Experimental research on discharge characteristics of LHT40 low power Hall thruster [J]. Chinese Space Science and Technology, 2021, 41(5): 65-74.
[9]	YAN Nengwen, GUO Ning, WU Chenchen, GU Zengjie, YANG Zhaolun. Research on RF-ion thruster based on discharge chamber uniform model [J]. Chinese Space Science and Technology, 2021, 41(3): 1-8.
[10]	GENG Hai, SUN Mingming, LUO Junhua, LIU Jiatao. Study on the thermal radiation influence of the sputtering target on the ion thruster [J]. Chinese Space Science and Technology, 2021, 41(2): 10-18.
[11]	WU Qinqin, LIU Xinyu, DENG Hanwen, KANG Xiaoming. Research status and prospect of chemical-electrospray dual-mode propulsion system [J]. Chinese Space Science and Technology, 2021, 41(1): 1-12.
[12]	YANG Sanxiang, LIU Chao, WANG Shangmin, FENG Jie, CHEN Juanjuan, WU Chenchen, JIA Yanhui, GUO Ning, GENG Hai . Numerical study of electromagnetic acceleration mechanism for pulsed plasma thruster [J]. Chinese Space Science and Technology, 2020, 40(4): 11-21.
[13]	CHEN Jie, KANG Xiaolu, ZHAO Zhen, CHENG Jiabing, LIANG Wei. High specific impulse Hall thruster startup characteristics [J]. Chinese Space Science and Technology, 2020, 40(4): 22-28.
[14]	DUAN Chuanhui, REN Lixin, CHANG Yajie, BAI Qian, AN Ran, HUANG Yusong. All electric propulsion satellite trajectory optimization by homotopic approach [J]. Chinese Space Science and Technology, 2020, 40(2): 42-.
[15]	YU Bo, ZHANG Min, YU Shui-Lin, KANG Xiao-Lu. Investigation of the Sband electromagnetic wave attenuation by the Hall thruster plume [J]. Chinese Space Science and Technology, 2019, 39(5): 19-.

Study on moment dumpling of electric propulsion satellite

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments