A next-generation lunar lander Guidance, Navigation, and Control (GNC) system, which includes a state-of-the-art optical sensor suite, is proposed in a concept design cycle. The design goal is to allow the lander to softly land within the prescribed landing precision. The achievement of this precision landing requirement depends on proper selection of the sensor suite. In this paper, a robust sensor selection procedure is demonstrated using a Linear Covariance (LinCov) analysis tool developed by Draper.
Linear Covariance Analysis for a Lunar Lander
AIAA SciTech 2017 Conference ; 2017 ; Grapevine, TX, United States
2017-01-09
Conference paper
No indication
English
Linear Covariance Analysis for a Lunar Lander
AIAA | 2017
|DataCite | 2024
|ASCE | 2008
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Online Contents | 2009
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