An approach to dynamics of flexible orbiting systems with application to the proposed space station
Author:
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference24 articles.
1. Direct path method for flexible multibody spacecraft dynamics;Ho;J. Spacecraft Rockets,1977
2. Dynamics of flexible bodies in tree topology—a computer-oriented approach;Singh;J. Guidance Control Dynam.,1985
3. Equations of motion for maneuvering flexible spacecraft;Meirovitch;J. Guidance Control Dynam.,1987
4. Dynamics of Earth-orbiting flexible satellites with multibody components;Vu-Quoc;J. Guidance Control Dynam.,1987
5. Selection of component modes for the simulation of flexible multibody spacecraft;Spanos,1989
Cited by 3 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. Dynamics of a flexible platform due to operational disturbances;Acta Astronautica;1999-01
2. Man, the unknown: fleeting impressions of an uncertain mindBREAKWELL MEMORIAL LECTURE;Acta Astronautica;1997-07
3. Control-structure interaction study of the proposed space station freedom;Acta Astronautica;1993-12
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