A Dynamics and Control Algorithm for Low Earth Orbit Precision Formation Flying Satellites

A Dynamics and Control Algorithm for Low Earth Orbit Precision Formation Flying Satellites

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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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Bibliographic Details
Main Author: Eyer, Jesse
Other Authors: Damaren, Christopher John
Language:en_ca
Published: 2009
Subjects:
Formation flying
Dynamics and control
0538
Online Access:http://hdl.handle.net/1807/19186

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