Thermally induced vibrations of a flexible appendage attached to a spacecraft
Author:
Affiliation:
1. Mitsubishi Electric Corp., Amagasaki, Hyogo, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.7344
Reference12 articles.
1. On the high-spin motion of a satellite containing elastic parts.
2. A Comparative Study of Stability Methods for Flexible Satellites
3. Attitude Stability of a Dual-Spin Satellite with a Large Flexible Solar Array
4. Liapunov stability analysis of spinning flexible spacecraft.
5. 5Pringle, R., Jr. "Stability of the Force-Free Motions of a Dual-Spin Spacecraft,'M/A4 Journal, Vol.7, June 1969, pp.1054-1063.
Cited by 10 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. Thermo-Mechanical Jitter in Slender Space Structures: A Simplified Modeling Approach;Aerospace;2024-08-25
2. Breakwell Memorial Lecture: Attitude dynamics of satellite—From spinning satellite to space robot;Acta Astronautica;2008-01
3. Attitude Dynamics of Satellites: from Spinning Sat...;56th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law;2005-10-17
4. Thermally Induced Vibrations of Spinning Thin-Walled Composite Beam;AIAA Journal;2003-02
5. Thermally Induced Vibrations of Spinning Composite Structures;43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2002-04-22
1.学者识别学者识别
2.学术分析学术分析
3.人才评估人才评估
"同舟云学术"是以全球学者为主线，采集、加工和组织学术论文而形成的新型学术文献查询和分析系统，可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容，当前同舟云学术共收录了国内外主流学术期刊6万余种，收集的期刊论文及会议论文总量共计约1.5亿篇，并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询！咨询电话：010-8811{复制后删除}0370
www.globalauthorid.com
TOP
Copyright © 2019-2024 北京同舟云网络信息技术有限公司 京公网安备11010802033243号 京ICP备18003416号-3