Mars Precision Entry Vehicle Guidance Using Internal Moving Mass Actuators
Many landing sites of scientific interest on Mars including most of the Southern Hemisphere at elevations above 2km Mars Orbiter Laser Altimeter reference are inaccessible due to current limitations in precision entry guidance and payload deceleration. Precision guidance and large payload decelerati...
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Virginia Tech
2014
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| Online Access: | http://hdl.handle.net/10919/50648 |