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Optical Navigation Method and Error Analysis for the Descending Landing Phase in Planetary Exploration

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 an imaging cosine equivalent mathematical model bas...

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Principais autores: Rongjun Mu, Peng Wu, Yanpeng Deng, Haofan Song
Format: Artigo
Sprog:Inglês
Udgivet: MDPI AG 2022-09-01
Serier:Aerospace
Fag:
optical navigation
crater detection algorithm
spatial position distribution
torus
lunar exploration
Online adgang:https://www.mdpi.com/2226-4310/9/9/496
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