Backstepping attitude coordination control for spacecraft formation with multiple delays

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Abstract

This paper addresses attitude coordination control for spacecraft formation with multiple delays. A distributed angular velocity input law is firstly constructed for attitude synchronization and tracking under multiple communication delays. Introducing virtual auxiliary systems makes it possible to integrate the angular velocity input law with the true control torque, and asymptotic stability of the system is guaranteed by Lyapunov theory. Moreover, by modifying the angular velocity input law, attitude coordination among spacecrafts can be guaranteed even under control input saturation constraints. Finally, effectiveness of the proposed methodology is illustrated by concrete simulations.

Original languageEnglish
Title of host publication2nd IAA Conference on Dynamics and Control of Space Systems, 2014
EditorsFilippo Graziani, Anna D. Guerman, Jean-Michel Contant
PublisherUnivelt Inc.
Pages1043-1054
Number of pages12
ISBN (Print)9780877036173
Publication statusPublished - 2015
Event2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014 - Rome, Italy
Duration: 24 Mar 201426 Mar 2014

Publication series

NameAdvances in the Astronautical Sciences
Volume153
ISSN (Print)0065-3438

Conference

Conference2nd International Academy of Astronautics Conference on Dynamics and Control of Space Systems, DyCoSS 2014
Country/TerritoryItaly
CityRome
Period24/03/1426/03/14

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