The Effect of Navigation State Selection on Fuel Dispersions for Powered Lunar Descent
A Monte Carlo simulation is developed to study the performance of the closed-loop guidance, navigation, and control (GN&C) system of a lunar lander in powered descent. The simulation includes six-degrees-of-freedom dynamics, an extended Kalman �lter, guidance based upon modi�ed Apollo methods, a...
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| Format: | Others |
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DigitalCommons@USU
2013
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| Online Access: | https://digitalcommons.usu.edu/etd/2004 https://digitalcommons.usu.edu/cgi/viewcontent.cgi?article=3007&context=etd |