Simultaneous estimation of spacecraft position and asteroid diameter during final approach of Hayabusa2 to Ryugu (vol 4, pg 163, 2020)

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Takao, Y.

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ASTRODYNAMICS | 2022年 / 6卷 / 04期

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V [航空、航天];

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08 ; 0825 ;

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页码：441 / 441

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[6] Rendezvous to asteroid with highly uncertain ephemeris: Hayabusa2s Ryugu-approach operation result (vol 4, pg 137, 2020)
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[7] Image-based autonomous navigation of Hayabusa2 using artificial landmarks: The design and brief in-flight results of the first landing on asteroid Ryugu (vol 4, pg 89, 2020)
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[9] Orbit insertion strategy of Hayabusa2s rover with large release uncertainty around the asteroid Ryugu (vol 4, pg 309, 2020)
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ASTRODYNAMICS, 2022, 6 (04) : 442 - 442
[10] Design and flight results of GNC systems in Hayabusa2 descent operations (vol 4, pg 105, 2020)
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