LIMITS ON THE DAMPING OF TWO-BODY GRAVITATIONALLY ORIENTED SATELLITES
Author:
Affiliation:
1. Bell Telephone Laboratories, Inc., Murray Hill, N. J.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.1587
Reference11 articles.
1. Damping of a Gravitationally Oriented Two-Body Satellite
2. Kamm, L. J. "Vertistat: an improved satellite orientation device/7ARSJ. 32, 911-913 (1962).
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Decay rates of a passive precession damper and bounds.;Journal of Spacecraft and Rockets;1966-03
2. A Two-Gyro, Gravity-Gradient Satellite Attitude Control System;Bell System Technical Journal;1964-11
3. Decay rates of passive precession dampers and their bounds;Astrodynamics Guidance and Control Conference;1964-08-16
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