Attitude Dynamics/Control of a Dual-Body Spacecraft with Variable-Speed Control Moment Gyros

Author:

Romano Marcello1,Agrawal Brij N.1

Affiliation:

1. Naval Postgraduate School, Monterey, California 93943

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

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