Attitude Control Technology of Upper Stage During Orbital Transfer

doi:10.3780/j.issn.1000-758X.2014.05.006

Chinese Space Science and Technology ›› 2014, Vol. 34 ›› Issue (5): 41-48,55.doi: 10.3780/j.issn.1000-758X.2014.05.006

Previous Articles Next Articles

Attitude Control Technology of Upper Stage During Orbital Transfer

WANG Zhao-Hui¹, JIN Lei¹, JIA Ying-Hong¹, DUAN Jia-Jia²

(1BeijingUniversityofAeronauticsandAstronautics，Beijing100191)
(2ShanghaiInstituteofAerospaceControlTechnology，Shanghai100048)

Received:2014-02-18 Revision received:2014-05-16 Online:2014-10-25 Published:2014-10-25

Abstract

Abstract: A method which providing three-axis attitude control by the gimbaled thruster gimbal and yaw attitude control thruster was proposed. Firstly, the multi-body dynamics equations with the upper stage body, gimbaled thruster and gimbal support were built based on the Kane equation. The gimbaled thruster′s disturbance torque and gimbal angle formulas when the gimbaled thruster working were derived. Sceondly, the upper stage attitude control law was designed based on the variable structure control law, that not only achieved 10^-3 atttiude control precision, but allowed the gimbaled thruster′s thrust direction achieve the direction determined by the guidance system as well as was via the mass center of upper stage. Finally, the validity of the proposed method was verified by numerical simulations.

Key words: Variable structure control, Gimbaled thruster, Orbital transfer, Attitude control

WANG Zhao-Hui, JIN Lei, JIA Ying-Hong, DUAN Jia-Jia. Attitude Control Technology of Upper Stage During Orbital Transfer[J]. Chinese Space Science and Technology, 2014, 34(5): 41-48,55.

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

URL: https://journal26.magtechjournal.com/kjkxjs/EN/10.3780/j.issn.1000-758X.2014.05.006

https://journal26.magtechjournal.com/kjkxjs/EN/Y2014/V34/I5/41

[1]	. Staring mode attitude control of Geo-SAR satellite with reflector antenna [J]. Chinese Space Science and Technology, 2025, 45(3): 100-109.
[2]	ZHANG Honghua, GUAN Yifeng, LI Ji, YU Jie, CHEN Yao, WANG Zhiwen, ZHANG Xiaowen, ZHANG Luchen, LI Linfeng, SUN Guojian, WANG Zhenhua, GUO Minwen, LI Xiaofeng, GAO Xizhen. A dual-loop fault tolerant attitude control for the Chang′e-6 lunar orbit flight [J]. Chinese Space Science and Technology, 2024, 44(5): 15-22.
[3]	LEI Yongjun, LU Dongning, YUAN li, CHEN chao. An attitude control method of satellites with hybrid flywheel configuration for skew maneuvers [J]. Chinese Space Science and Technology, 2024, 44(3): 111-119.
[4]	YUAN Quan, LIN Hanzheng, ZHANG Jun, WEI Chunling. Attitude maneuver and physical test of large-scale spacecraft with ultra-low frequency [J]. Chinese Space Science and Technology, 2022, 42(1): 57-64.
[5]	YAN Nanxing, LIN Zhe, LIU Yaning, YU Fei, WANG Chun, KANG Jianbing. Research on satellite optical axis compound pointing control method [J]. Chinese Space Science and Technology, 2021, 41(3): 114-122.
[6]	LEI Yongjun, Yuan Li, LIU Qirui, LIU Jie. An attitude hybrid control method for earth-orienting satellite systems with 2-SGCMGs and magnet torquers [J]. Chinese Space Science and Technology, 2021, 41(1): 75-83.
[7]	GENG Feilong, LI Shuang, HUANG Xuxing, YANG Bin, CHANG Jiansong, LIN Bo. Fault diagnosis and fault tolerant control of spacecraft attitude control system via deep neural network [J]. Chinese Space Science and Technology, 2020, 40(6): 1-12.
[8]	WU Jiaqi, KANG Guohua, HUA Yinmiao, ZHANG Han, ZHANG Qi. Research on intelligent cooperative attitude control of assembled spacecraft#br# [J]. Chinese Space Science and Technology, 2020, 40(4): 44-53.
[9]	YANG Bo, ZHU Yichuan, WEI Yanming, FAN Zichen. Trajectory optimization and control analysis of folding wing aircraft [J]. Chinese Space Science and Technology, 2020, 40(3): 64-75.
[10]	XU Ying, ZHANG Jin, YU Moyao, XU Dandan. Attitude and orbit coupling control for fly-around observation of multi-satellite proximity operation [J]. Chinese Space Science and Technology, 2019, 39(6): 21-.
[11]	YANG Chi-Hang, LIU Jiang-Kai, LONG Long- , SONG Huan, LI Long, ZHU Ling-Chao, YE Bing-Xu, CHEN Hong-Ru, ZHANG Hao. Preliminary design and test of attitude control system for lunar CubeSats [J]. Chinese Space Science and Technology, 2019, 39(4): 28-.
[12]	WANG Yue-Jiao, MA Zhong, YANG Yi-Dai, WANG Zhu-Ping, TANG Lei. Satellite attitude control method based on deep reinforcement learning [J]. Chinese Space Science and Technology, 2019, 39(4): 36-.
[13]	YANG Wulin, CHEN Chuan, YU Qian, LI Ming, GONG Zizheng. Research and development of simulation platform for orbital debris removal with spacebased laser system [J]. Chinese Space Science and Technology, 2019, 39(1): 59-.
[14]	ZHANG Henghao, TANG Qingbo, YAN Ning, CHEN Chunyan, ZHENG Zhenglu. Intelligent fuzzy control algorithm of flexible spacecraft [J]. Chinese Space Science and Technology, 2018, 38(4): 36-43.
[15]	ZHANG Ke-Bei, WANG Da-Yi, TANG Liang, WANG You-Yi. Gyrofree spacecraft attitude layered control based on observer [J]. Chinese Space Science and Technology, 2017, 37(6): 24-.

Attitude Control Technology of Upper Stage During Orbital Transfer

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments