Cascade-Based Controlled Attitude Synchronization and Tracking of Spacecraft in Leader-Follower Formation

The authors of this study propose controllers for leader-follower attitude synchronization of spacecraft formations in the presence of disturbances, that is, the leader spacecraft is controlled to follow a given reference, while a follower spacecraft is controlled to synchronize its motion with the leader's. In the ideal disturbance-free scenario, the authors show that synchronization takes place asymptotically. Moreover, they show the property of uniform practical asymptotic stability which implies that the synchronization is robust to bounded disturbances.

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  • English

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  • Accession Number: 01344951
  • Record Type: Publication
  • Files: TRIS
  • Created Date: Jul 20 2011 7:24AM