PMO OpenIR  > 空间目标与碎片观测研究基地
Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque
Zhang, Ming-Jiang1,2,3; Zhao, Chang-Yin1,2
2015-02-01
Source PublicationASTROPHYSICS AND SPACE SCIENCE
Volume355Issue:2Pages:203-212
AbstractThe attitude stability of a dual-spin spacecraft on a stable stationary orbit around an asteroid subjected to gravity gradient torque is studied in this paper, in which the effect of the second order and degree harmonics C-20 and C-22 of the gravity field of the asteroid is involved. Under some reasonable assumptions, the linearized equations of attitude motion of the dual-spin spacecraft with a nutation damper are presented. Then the necessary and sufficient conditions of attitude stability of the dual-spin spacecraft with a nutation damper are derived. Meantime, the linearized equations of attitude motion and the conditions of attitude stability of the dual-spin spacecraft without a nutation damper are also presented. These results are generalized and encompass a series of special cases, and from which some useful conclusions on the attitude stability of the dual-spin spacecraft are obtained. Examples are given to illustrate the application of these conditions of attitude stability.
KeywordAttitude Stability Dual-spin Spacecraft Asteroid Conditions Of Stability
Subject Area天文和天体物理
WOS HeadingsScience & Technology ; Physical Sciences
DOI10.1007/s10509-014-2145-y
WOS KeywordEQUILIBRIUM ATTITUDE ; DYNAMICS
Indexed BySCI
Language英语
WOS Research AreaAstronomy & Astrophysics
WOS SubjectAstronomy & Astrophysics
WOS IDWOS:000350206600001
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Document Type期刊论文
Identifierhttp://libir.pmo.ac.cn/handle/332002/14817
Collection空间目标与碎片观测研究基地
Affiliation1.Chinese Acad Sci, Purple Mt Observ, Nanjing 210008, Jiangsu, Peoples R China
2.Chinese Acad Sci, PMO, Key Lab Space Object & Debris Observat, Nanjing 210008, Jiangsu, Peoples R China
3.Univ Chinese Acad Sci, Beijing 100049, Peoples R China
Recommended Citation
GB/T 7714
Zhang, Ming-Jiang,Zhao, Chang-Yin. Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque[J]. ASTROPHYSICS AND SPACE SCIENCE,2015,355(2):203-212.
APA Zhang, Ming-Jiang,&Zhao, Chang-Yin.(2015).Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque.ASTROPHYSICS AND SPACE SCIENCE,355(2),203-212.
MLA Zhang, Ming-Jiang,et al."Attitude stability of a dual-spin spacecraft on a stationary orbit around an asteroid subjected to gravity gradient torque".ASTROPHYSICS AND SPACE SCIENCE 355.2(2015):203-212.
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