Evaluation of microgravity level fluctuation due to attitude/orbital motion in a tethered satellite system-Reference-Cited by-同舟云学术

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Evaluation of microgravity level fluctuation due to attitude/orbital motion in a tethered satellite system

Published:1995-01 Issue:2-3 Volume:35 Page:187-191
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Ohkami Yoshiaki,Yoshimura Shoichi,Okamoto Osamu

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference5 articles.

1. Applications of tethers in space;NASA;NASA CP 2422,1985

2. A three-mass system for micro-g/variable-g applications;Lorentini;AIAA/AAS GNCC, No. 86-1990,1986

3. Frequencies of longitudinal oscillation of tethered satellite systems;Misra,1986

4. Effects of tether flexibility on the tethered shuttle substellite stability and control;Liangdong;J. Guid.,1989

5. A parameteric study of the tethered-elevator dynamics and control in the presence of attaching point offset;Modi;IAF-91-355,1991

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. Method to maintain artificial gravity during transfer maneuvers for tethered spacecraft;Acta Astronautica;2016-03

2. Research of Dynamics and Deploying Control Method on Tethered Satellite;Proceedings of International Conference on Soft Computing Techniques and Engineering Application;2013-12-21

3. Dynamic multibody modeling for tethered space elevators;Acta Astronautica;2009-08

4. A review of space tether research;Progress in Aerospace Sciences;2008-01

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