Numerical Analysis of Relative Orbit Control Strategy for CANYVAL-X Mission

Numerical Analysis of Relative Orbit Control Strategy for CANYVAL-X Mission

This paper suggests a relative orbit control strategy for the CubeSat Astronomy by NASA and Yonsei using Virtual Telescope Alignment eXperiment (CANYVAL-X) mission whose main goal is to demonstrate an essential technique, which is an arrangement among two satellites and a specific celestial object,...

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Bibliographic Details
Main Authors: Lee, Youngro, Park, Sang-Young, Park, Jae-Pil, Song, Youngbum
Format: Article
Language:English
Published: The Korean Space Science Society 2019-12-01
Series:Journal of Astronomy and Space Sciences
Subjects:
canyval-x
inertial alignment
inertial alignment system
relative orbit control
proximity keeping
reconfiguration
Online Access:https://doi.org/10.5140/JASS.2019.36.4.235

Internet

https://doi.org/10.5140/JASS.2019.36.4.235

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