Kaito Ariu

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Abstract: This paper summarizes the development of and initial flight results relating to the attitude determination and control system of PROCYON, which is the world’s first micro-spacecraft that is capable of deep space missions. Because success in the automatic attitude control sequence from separation to sun pointing on the launch day is critical for(More)
This paper describes a relative orbit estimation method for the close distance flyby adjacent to small bodies such as asteroids, comets, and natural satellites. Previous studies showed that, in a high-speed relative velocity flyby or a close distance flyby of small astronomical bodies, typical estimation algorithms such as a linear batch processing and an(More)
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