Dynamic Modeling and Attitude Control of Large-Scale Flexible Parallel Multibody Spacecraft
Author:
Affiliation:
1. Nanjing University of Aeronautics and Astronautics, 211106 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.G007137
Reference26 articles.
1. Equivalent Dynamic Model of the Space Antenna Truss with Initial Stress
2. Deployment dynamics and control of large-scale flexible solar array system with deployable mast
3. Numerical and experimental investigation on dynamics of deployable space telescope experiencing deployment and attitude adjustment motions coupled with laminated composite shell
4. Deployment dynamics for flexible deployable primary mirror of space telescope with paraboloidal and laminated structure by using absolute node coordinate method
5. Multibody dynamic simulation of the next generation space telescope using finite elements and fuzzy sets
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