Frequencies of longitudinal oscillations of tethered satellite systems-Reference-Cited by-同舟云学术

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Frequencies of longitudinal oscillations of tethered satellite systems

Published:1986-08-17 Issue: Volume: Page:
ISSN:
Container-title:Astrodynamics Conference
language:
Short-container-title:

Author:

MISRA A.¹,MODI V.²

Affiliation:

1. McGill University, Montreal, Canada

2. British Columbia, University, Vancouver, Canada

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1986-2274

Reference9 articles.

1. 2.1628 2.1556 2.1542 2.1535 2.1532

2. Control of Non-Rigid Spacecraft, Frascati, F Italy, May 1976, pp. 349-354.

3. Two Satellites Connected by a Deployable and Extensible Tether of Finite Mass", Contract Report, ESTEC Contract No. 2992/76/NL/AK(SC), Vols. 1 and 2, October 1978. Mode I 2 3 4 5

Cited by 4 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. Evaluation of microgravity level fluctuation due to attitude/orbital motion in a tethered satellite system;Acta Astronautica;1995-01

2. Insights and approximations in dynamic analysis of spacecraft tethers;Dynamics Specialists Conference;1990-04-05

3. Insights And Approximations In Dynamic Analysis Of Spacecraft Tethers;Mechanics And Control Of Large Flexible Structures;1990-01-01

4. Some approximations for the dynamics of spacecraft tethers;28th Structures, Structural Dynamics and Materials Conference;1987-04-06

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