Eigenvalues and eigenvectors for hybrid coordinate equations of motion for flexible spacecraft-Reference-Cited by-同舟云学术

Eigenvalues and eigenvectors for hybrid coordinate equations of motion for flexible spacecraft

Published:1979-05 Issue:4 Volume:19 Page:359-390
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Ohkami Yoshiaki,Likins Peter

Publisher

Springer Science and Business Media LLC

Subject

General Medicine,Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modeling and Simulation

Link

http://link.springer.com/content/pdf/10.1007/BF01231015.pdf

Reference6 articles.

1. Likins, P. W.: 1970, ?Dynamics and Control of Flexible Space Vehicles?, TR32-1329, Rev. 1, Jet Propulsion Laboratory.

2. Ohkami, Y. and Likins, P. W.: (1974), ?The Influence of Spacecraft Flexibility on System Controllability and Observability?, presented at the 6th IFAC symposium on Automatic Control in Space, U.S.S.R., August 1974.

3. Wilkinson, J. H.: 1965,The Algebraic Eigenvalue Problem, Clarendon Press, Oxford, pp. 94?109.

4. Gantmacher, F. R.: 1959,The Theory of Matrices, Vol. 1, Chelsea, pp. 45?46, pp. 250?256.

5. Hughes, P. C.: 1974,Celest. Mech. 9, 21?39.

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