Dynamic Modeling and Distributed Control of Asymmetric Flexible Spacecraft
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 210016 Nanjing, People’s Republic of China
2. University of Missouri, Columbia, Missouri 65211
Funder
National Natural Science Foundation of China
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
https://arc.aiaa.org/doi/pdf/10.2514/1.G006919
Reference24 articles.
1. Dynamics and on-orbit assembly strategies for an orb-shaped solar array
2. Modeling and neural network control of a flexible beam with unknown spatiotemporally varying disturbance using assumed mode method
3. An anti-disturbance PD control scheme for attitude control and stabilization of flexible spacecrafts
4. On-Orbit Robust Control Experiment of Flexible Spacecraft ETS-VI
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