EQUILIBRIUM ORIENTATIONS OF GRAVITY-GRADIENT SATELLITES
Author:
Affiliation:
1. Illinois Institute of Technology, Chicago, Ill.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1583
Reference6 articles.
1. On the Crack-Tip Stress-Intensity Factors for Cylindrical Bars Under Torsion
2. The torsion and flexure of shafting with keyways or cracks
3. May 1960;Beletskiy V. V.,1959
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1. Satellite attitude stabilization through tether;Acta Astronautica;1995-03
2. Satellite attitude dynamics and control in the presence of environmental torques - A brief survey;Journal of Guidance, Control, and Dynamics;1983-11
3. Satellite attitude dynamics and control in presence of environmentaltorques - A brief survey;Astrodynamics Conference;1982-08-09
4. Gravity field exploration by a new gradient technique.;Journal of Spacecraft and Rockets;1969-06
5. A new type of space exploration by gradient technique;Control and Flight Dynamics Conference;1968-08-12
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