Aerodynamic passive stabilization design and flight data analyses for transitional regime satellite LX-1

doi:10.1016/j.actaastro.2019.11.011

	Aerodynamic passive stabilization design and flight data analyses for transitional regime satellite LX-1
	Xuegang, Zhang 1,2,3; Zhencai, Zhu2,4 ; Hongyu, Chen2,4
	2020-02
发表期刊	ACTA ASTRONAUTICA (IF:3.1[JCR-2023],3.1[5-Year])
ISSN	0094-5765
卷号	167 页码:232-238
发表状态	已发表
DOI	10.1016/j.actaastro.2019.11.011
摘要	The transitional regime satellite LX-1, was designed by the Innovation Academy for Microsatellites Chinese Academy of Sciences (IAMCAS) to conduct research on transitional regime rarefied gas. The LX-1 successfully stabilized attitudes by aerodynamic torque for more than 72 h. It featured the lowest orbit altitude between 110km and 130km of every active spacecraft and firstly confirmed aerodynamic passive stabilization design was feasible for transitional regime satellites. In the paper, the authors revealed the design methods, including stability analyses and design details in LX-1. As well, the presented flight data of LX-1 demonstrated that the design displayed the capability to maintain attitude better than 10^∘ and 0.5^∘/s for the transitional regime satellite. Further studies suggested that the design could simplify control system design, reduce the propellant requirement for active attitude control and prolong the satellite's lifetime. Therefore, aerodynamic passive stabilization design had considerable potential in aerospace engineering and the study could provide the experience for further research. © 2019 IAA
收录类别	EI ; SCIE ; SCI
出版者	Elsevier Ltd
EI入藏号	20194707719684
EI主题词	Aerodynamics ; Attitude control ; Control systems ; Design ; Flight control systems ; Orbits ; Satellites ; Spacecraft propulsion ; Stabilization ; Systems analysis
EI分类号	Aerodynamics:651 ; Aerodynamics, General:651.1 ; Satellites:655.2 ; Space Flight:656.1 ; Control Systems:731.1 ; Specific Variables Control:731.3 ; Systems Science:961
原始文献类型	Journal article (JA)
引用统计	正在获取...
文献类型	期刊论文
条目标识符	https://kms.shanghaitech.edu.cn/handle/2MSLDSTB/104322
专题	信息科学与技术学院_特聘教授组_朱振才组信息科学与技术学院_特聘教授组_陈宏宇组
通讯作者	Xuegang, Zhang
作者单位	1.Shanghai Institute of Microsystem and Information Technology, Chinese Academy of Sciences, Shanghai; 200050, China 2.Innovation Academy for Microsatellites, Chinese Academy of Sciences, Shanghai; 201203, China 3.University of Chinese Academy of Sciences, Beijing; 100049, China 4.School of Information Science and Technology, ShanghaiTech University, Shanghai; 201210, China
推荐引用方式 GB/T 7714	Xuegang, Zhang,Zhencai, Zhu,Hongyu, Chen. Aerodynamic passive stabilization design and flight data analyses for transitional regime satellite LX-1[J]. ACTA ASTRONAUTICA,2020,167:232-238.
APA	Xuegang, Zhang,Zhencai, Zhu,&Hongyu, Chen.(2020).Aerodynamic passive stabilization design and flight data analyses for transitional regime satellite LX-1.ACTA ASTRONAUTICA,167,232-238.
MLA	Xuegang, Zhang,et al."Aerodynamic passive stabilization design and flight data analyses for transitional regime satellite LX-1".ACTA ASTRONAUTICA 167(2020):232-238.