Asteroid rotation and orbit control via laser ablation

This paper presents an approach to control the rotational motion of an asteroid while a spacecraft is deflecting its trajectory through laser ablation. During the deflection, the proximity motion of the spacecraft is coupled with the orbital and rotational motion of the asteroid. The combination of...

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Bibliographic Details
Main Authors: Vetrisano, Massimo (Author), Colombo, Camilla (Author), Vasile, Massimiliano (Author)
Format: Article
Language:English
Published: 2015-07-03.
Subjects:
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