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Optical Navigation System for Pin-Point Lunar Landing
2014
IFAC Proceedings Volumes
Major space agencies have an increasing interest in highly accurate (200 m) autonomous landing on the Moon. Inertial-only navigation is not compatible with this challenging requirement. The techniques currently investigated rely on vision-based navigation. A first approach consists in tracking features between sequences of images in order to measure the angular rate as well as the direction of the velocity vector of the spacecraft. A second approach aims at identifying image features using a
doi:10.3182/20140824-6-za-1003.01693
fatcat:2fsnnnarmbgofmmsalaqsh2tta