A two-degree-of-freedom control moment gyro for high-accuracy attitude control.-Reference-Cited by-同舟云学术

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A two-degree-of-freedom control moment gyro for high-accuracy attitude control.

Published:1968-01 Issue:1 Volume:5 Page:74-83
ISSN:0022-4650
Container-title:Journal of Spacecraft and Rockets
language:en
Short-container-title:Journal of Spacecraft and Rockets

Author:

LISKA DONALD J.¹

Affiliation:

1. University of California, Los Alamos Scientific Laboratory, Los Alamos, N. Mex.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/3.29188

Reference7 articles.

1. Effect of gravity gradient on attitude control of a space station

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1. Torque distribution of The Integrated Magnetically Suspended Inertia Actuator for attitude maneuvers;Acta Astronautica;2016-02

2. Control moment gyroscopes for spacecraft attitude control systems: Current status and prospects;Gyroscopy and Navigation;2015-07

3. Energetics of Control Moment Gyroscopes as Joint Actuators;Journal of Guidance, Control, and Dynamics;2009-11

4. Scissored-Pair Control-Moment Gyros: A Mechanical Constraint Saves Power;Journal of Guidance, Control, and Dynamics;2008-11

5. Control Moment Gyros as Space-Robotics Actuators;AIAA Guidance, Navigation and Control Conference and Exhibit;2008-06-15

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