Analytical solution of attitude motion for spacecraft with a slewing appendage-Reference-Cited by-同舟云学术

Analytical solution of attitude motion for spacecraft with a slewing appendage

Published:1994-09 Issue:2 Volume:6 Page:193-214
ISSN:0924-090X
Container-title:Nonlinear Dynamics
language:en
Short-container-title:Nonlinear Dyn

Author:

Shen Q.,Soudack A. C.,Modi V. J.

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Applied Mathematics,Mechanical Engineering,Ocean Engineering,Aerospace Engineering,Control and Systems Engineering

Link

http://link.springer.com/content/pdf/10.1007/BF00044985.pdf

Reference14 articles.

1. Turner, J. D. and Junkins, J. L., ‘Optimal large-angle single axis rotational maneuver of flexible spacecraft’, Journal of Guidance and Control 3, 1980, 578–585.

2. Mah, H. W. and Modi, V. J., ‘Dynamics and control during slew maneuvers’, Acta Astronautica 19, 1989, 125–143.

3. Bainum, P. M. and Li, F., ‘Rapid in-plane maneuvering of the flexible orbiting SCOLE’, The Journal of the Astronautical Science 39, 1991, 233–248.

4. Meirovitch, L. and Quinn, R. D., ‘Equations of motion for maneuvering flexible spacecraft’, Journal of Guidance, Control, and Dynamics 10, 1987, 453–465.

5. Meirovitch, L. and Kwak, M. K., ‘On the maneuvering and control of space structures’, in The Dynamics of Flexible Structures in Space, C. L. Kirk and J. L. Junkins (eds.), Springer-Verlag, Berlin, 1990, 3–17.

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