Possible effects of boom flutter on the attitude dynamics of the OV1-10 satellite.-Reference-Cited by-同舟云学术

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Possible effects of boom flutter on the attitude dynamics of the OV1-10 satellite.

Published:1969-01 Issue:1 Volume:6 Page:90-92
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

CONNELL G. M.¹,CHOBOTOV V.¹

Affiliation:

1. Aerospace Corporation, El Segundo, Calif.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.29542

Reference4 articles.

Cited by 11 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. Experimental Verification of the Thermal Flutter Criterion for a Slender Cantilever Boom;AIAA Journal;2022-08

2. A thermal-flutter criterion for an open thin-walled circular cantilever beam subject to solar heating;Chinese Journal of Aeronautics;2018-09

3. Stability of Thermally Induced Vibration of a Beam Subjected to Solar Heating;AIAA Journal;2014-03

4. Attitude Error of Satellite Due to Gravity Gradient Boom;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2003

5. Control boom design of Z-SAT;Modeling and Simulation Technologies Conference;2000-08-14

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