Inertia-free minimum-angular-motion detumbling control of spacecraft

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

8 Scopus citations

Original language	English
Pages (from-to)	678-683
Number of pages	6
Journal	Journal of Guidance, Control, and Dynamics
Volume	42
Issue number	3
DOIs	https://doi.org/10.2514/1.G003813
State	Published - 2019

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title = "Inertia-free minimum-angular-motion detumbling control of spacecraft",

author = "Xiao Feng and Yinghong Jia and Shijie Xu",

year = "2019",

doi = "10.2514/1.G003813",

language = "英语",

volume = "42",

pages = "678--683",

journal = "Journal of Guidance, Control, and Dynamics",

issn = "0731-5090",

publisher = "American Institute of Aeronautics and Astronautics Inc. (AIAA)",

number = "3",

}

TY - JOUR

T1 - Inertia-free minimum-angular-motion detumbling control of spacecraft

AU - Feng, Xiao

AU - Jia, Yinghong

AU - Xu, Shijie

PY - 2019

Y1 - 2019

UR - https://www.scopus.com/pages/publications/85061790832

U2 - 10.2514/1.G003813

DO - 10.2514/1.G003813

M3 - 文章

AN - SCOPUS:85061790832

SN - 0731-5090

VL - 42

SP - 678

EP - 683

JO - Journal of Guidance, Control, and Dynamics

JF - Journal of Guidance, Control, and Dynamics

IS - 3

ER -