Specifications of Spacecraft Flexible Appendage Rigidity-Reference-Cited by-同舟云学术

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Specifications of Spacecraft Flexible Appendage Rigidity

Published:1978-11 Issue:6 Volume:1 Page:427-432
ISSN:0162-3192
Container-title:Journal of Guidance and Control
language:en
Short-container-title:Journal of Guidance and Control

Author:

Seltzer S.M.,Shelton H.L.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

General Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.21068

Reference4 articles.

1. ^iljak, D.D., Nonlinear Systems, John Wiley and Sons, New York, 1969, pp.1-106.

2. Hurty, W.C. and Rubinstein, M.F., Dynamics of Structures, Prentice-Hall, Englewood Cliffs, N.J., 1964, pp.110-140.

3. Low-Cost Space Telescope Pointing Control System

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Parameter-Plane Analysis for Large-Scale Systems;Journal of Guidance, Control, and Dynamics;1982-03

2. Parameter Plane Analysis for Large Flexible Spacecraft;Journal of Guidance, Control, and Dynamics;1981-05

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