Modeling and attitude control of CubeSat utilizing moving mass actuators-Reference-Cited by-同舟云学术

Modeling and attitude control of CubeSat utilizing moving mass actuators

Published:2021-01 Issue:1 Volume:67 Page:521-530
ISSN:0273-1177
Container-title:Advances in Space Research
language:en
Short-container-title:Advances in Space Research

Author:

Lu Zhengliang,Hu Yuandong^ORCID,Liao Wenhe,Zhang Xiang

Funder

National Natural Science Foundation of China

Natural Science Foundation of Jiangsu Province

Publisher

Elsevier BV

Subject

Space and Planetary Science,Aerospace Engineering,General Earth and Planetary Sciences,Atmospheric Science,Geophysics,Astronomy and Astrophysics

Reference18 articles.

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3. Chadwick, W.R., Malyevac, D.S., 2000. Considerations on the design of kinetic kill interceptor with moving mass control. Naval Surface Warfare Center, NSWCDD TR-00/87.

4. Faber, D., Overlack, A., Welland, W., et al., 2013. Nanosatellite deorbit motor. In: 27th Annual AIAA/USU Small Satellite Conference. SSC13-I-9.

5. Tactical Missile Design;Fleeman,2006

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