On-Orbit Robust Control Experiment of Flexible Spacecraft ETS-VI
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo 182, Japan
2. Toshiba Corporation, Kanagawa 210, Japan
3. National Space Development Agency, Ibaraki 305, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.4159
Reference21 articles.
1. Robust control design and implementation on the Middeck Active Control Experiment
2. Hubble Space Telescope pointing control system design improvement study results
3. Experimental modal analysis for dynamic models of spacecraft
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