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Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque
Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque
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Attitude stability of a spacecraft with two flexible solar arrays on a stationary orbit around an asteroid subjected to gravity gradient torque

Zhang, Ming-Jiang ; Zhao, Chang-Yin

Astrophysics and space science, 2014-06, Vol.351 (2), p.507-524 [Periódico revisado por pares]

Dordrecht: Springer Netherlands

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  • Realização: ABCD-USP USP   Logos de Redes Sociais: Freepik

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