Dynamics Modeling and Analysis of Spacecraft with Large Deployable Hoop-Truss Antenna-Reference-Cited by-同舟云学术

Dynamics Modeling and Analysis of Spacecraft with Large Deployable Hoop-Truss Antenna

Published:2016-05 Issue:3 Volume:53 Page:471-479
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

Liu Likun¹,Shan Jinjun²,Zhang Yan³

Affiliation:

1. China Academy of Space Technology, 100094 Beijing, People’s Republic of China

2. York University, Toronto, Ontario M3J 1P3, Canada

3. DFH Satellite Company, 100094 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.A33464

Reference18 articles.

1. WadeW. D.SinhaA.SinghR. “Final Report for Study of Wrap-Rib Antenna Design,” Lockheed Missiles and Space Co., Rept. NASA-CR-162929, Sunnyvale, CA, 1979.

2. Direct coordinate partitioning for multibody dynamics based on finite element method

3. AstroMesh Deployable Reflectors for Ku and Ka Band Commercial Satellites

4. A controlled deployment method for flexible deployable space antennas

5. Numerical form-finding of geotensoid tension truss for mesh reflector

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