A Dynamics and Control Algorithm for Low Earth Orbit Precision Formation Flying Satellites
An innovative dynamics and control algorithm is developed for a dual-nanosatellite formation flying mission. The principal function of this algorithm is to use regular GPS state measurements to determine the controlled satellite's tracking error from a set of reference trajectories in the local...
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| Language: | en_ca |
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2009
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| Online Access: | http://hdl.handle.net/1807/19186 |
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