An analysis of a single-burn algorithm for low-earth orbit maintenance
With the requirement for a spacecraft to maintain an orbital altitude band, a simple energy balance algorithm has been developed using a combination of radial distance and spacecraft specific energy for fixed-vector thruster control. While each trajectory produces a unique band, initial attempts at...
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Language: | en_US |
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Monterey, California. Naval Postgraduate School
2013
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Online Access: | http://hdl.handle.net/10945/30907 |