Avionics/Control co-design for large flexible space structures
Author:
Affiliation:
1. University of Toulouse
2. ONERA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2013-4638
Reference15 articles.
1. Robust Attitude Control Design for the BIOMASS Satellite (Earth Explorer Core Mission Candidate)
2. H∞ and LMI attitude control design: towards performances and robustness enhancement
3. Integrated design of system parameters, control and sensor/actuator placement for symmetric mechanical systems
4. Integrated optimal structural and vibration control design
5. An approach to structure/control simultaneous optimization for largeflexible spacecraft
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