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On the robust attitude regulation for earth observation spacecraft under hybrid actuation

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Abstract

Mission requirements for Earth observation spacecraft often influence the design philosophy of the latter and may additionally impose constraints and performance objectives on their attitude control functionality. We study the robust attitude regulation problem for such spacecraft, characterized primarily by hybrid actuation consisting of magnetic actuators and thrusters, assuming noisy attitude feedback. In our problem formulation, the angular accelerations induced by the attitude stabilization have to remain sufficiently small due to payload requirements. A linear robust control law is developed, which is tailored to the hybrid actuation scheme by appropriately complementing the directionally constrained magnetic torque with the thrusters.

Original languageEnglish
Title of host publicationSpaceflight Mechanics 2017
EditorsJon A. Sims, Frederick A. Leve, Jay W. McMahon, Yanping Guo
PublisherUnivelt Inc.
Pages2943-2960
Number of pages18
ISBN (Print)9780877036371
StatePublished - 2017
Externally publishedYes
Event27th AAS/AIAA Space Flight Mechanics Meeting, 2017 - San Antonio, United States
Duration: Feb 5 2017Feb 9 2017

Publication series

NameAdvances in the Astronautical Sciences
Volume160
ISSN (Print)0065-3438

Conference

Conference27th AAS/AIAA Space Flight Mechanics Meeting, 2017
Country/TerritoryUnited States
CitySan Antonio
Period02/5/1702/9/17

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