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pro vyhledávání: '"Haofan Song"'
Publikováno v:
Aerospace, Vol 9, Iss 9, p 496 (2022)
To solve the problem of high-precision optical navigation for the descent landing of lunar and planetary probes, an optical navigation method based on the spatial position distribution model is proposed. The method is based on crater detection, and a
Externí odkaz:
https://doaj.org/article/c3c951c40f77400b9d89ead2bc95d12b
