Orbit and attitude control for satellite formation flying

This thesis addresses the problems of orbit and attitude control for satellite formation flying. This thesis starts off with a comprehensive review of previous work related to trajectory optimization of formation maneuver, control strategy of formation keeping and attitude synchronization o...

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Bibliographic Details
Main Author: Wu, Baolin.
Other Authors: Wang Dan Wei
Format: Thesis
Language:English
Published: 2011
Subjects:
Online Access:http://hdl.handle.net/10356/46258