A Computational Intelligence Approach to the Mars Precision Landing Problem

A Computational Intelligence Approach to the Mars Precision Landing Problem

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Obstacles to reducing the landed footprint include trajectory dispersions due to initial atmospheric entry conditions (entry angle, parachute deployment height, etc.), environment (wind, atmospheric density, etc.), parachute deployment dynamics, unavoidable injection error (propagated error from launch on), etc. Weather and atmospheric models have been developed.Obstacles to reducing the landed footprint include trajectory dispersions due to initial atmospheric entry conditions (entry angle, parachute deployment height, etc.), environment (wind, atmospheric density, etc.), parachute deployment ...


Title:A Computational Intelligence Approach to the Mars Precision Landing Problem
Author:
Publisher:ProQuest - 2008
ISBN-13:

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