Effects of Orbital Perturbations on Deployment Dynamics of Tethered Satellite System Using Variable-Length Element

Orbital perturbations caused by the space environment will induce deviations compared with the prescribed motion trajectory or dynamic performance of the tethered satellite system (TSS). To comprehensively investigate the effects of the orbital perturbations on the TSS, a precise variable-length ele...

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Autors principals: Zhengfeng Bai, Xin Jiang
Format: Article
Idioma:English
Publicat: IEEE 2021-01-01
Col·lecció:IEEE Access
Matèries:
Accés en línia:https://ieeexplore.ieee.org/document/9344599/