Energy-Sink Analysis for Asymmetric Dual-Spin Spacecraft
Author:
Affiliation:
1. Ball Brothers Research Corporation, Boulder, Colo.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.62107
Reference13 articles.
1. Nutational stability of an axisymmetric body containing a rotor
2. Attitude stability criteria for dual spin spacecraft.
3. Attitude Stability of a Dual-Spin Satellite with a Large Flexible Solar Array
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2. Feedback Control Law Design for the Dual-Spin Turn of Spacecraft;Journal of Guidance, Control, and Dynamics;1997-05
3. Formulation of stability conditions for systems containing driven rotors;Journal of Guidance, Control, and Dynamics;1996-03
4. A spinning filled fluid reservoir for momentum biased spacecraft nutation damping;Control Engineering Practice;1994-10
5. Nutational stability and core energy of a quasirigid gyrostat;Journal of Guidance, Control, and Dynamics;1993-07
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