Multi-objective integrated robust H∞ control for attitude tracking of a flexible spacecraft

Author:

Wu Shunan,Chu Weimeng,Ma Xue,Radice Gianmarco,Wu Zhigang

Funder

National Natural Science Foundation of China

Central Universities

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Attitude and orbit control systems for the LISA Pathfinder mission;Giulicchi;Aero. Sci. Technol.,2013

2. Fluid ring damper for artificial gravity rotating system used for manned spacecraft;Gasbarri;Acta Astronaut.,2009

3. Constrained slews for single-axis pointing;Avanzini;J. Guidance, Control Dyn.,2008

4. Attitude control and vibration suppression for flexible spacecraft using control moment gyroscopes;Hu;J. Aero. Eng.,2015

5. Autonomous guidance for rendezvous phasing based on special-point-based maneuvers;Zhang;J. Guidance, Control, Dyn.,2015

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