Guidance and Navigation Linear Covariance Analysis for Lunar Powered Descent
A linear covariance analysis is conducted to assess closed-loop guidance, navigation, and control system (GN&C) performance of the Altair vehicle during lunar powered descent. Guidance algorithms designed for lunar landing are presented and incorporated into the closed-loop covariance equations...
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| Format: | Others |
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DigitalCommons@USU
2010
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| Online Access: | https://digitalcommons.usu.edu/etd/654 https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=1650&context=etd |