Study of Systems Using Inertia Wheels for Precise Attitude Control of a Satellite
Author: John S. White
Publisher:
Published: 1961
Total Pages: 78
ISBN-13:
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Author: John S. White
Publisher:
Published: 1961
Total Pages: 78
ISBN-13:
DOWNLOAD EBOOKAuthor: John S. White
Publisher:
Published: 1961
Total Pages: 44
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DOWNLOAD EBOOKAuthor: Stuart C. Brown
Publisher:
Published: 1961
Total Pages: 68
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DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1961
Total Pages: 1878
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DOWNLOAD EBOOKAuthor: John S. White (writer on artificial satellites.)
Publisher:
Published: 1961
Total Pages: 42
ISBN-13:
DOWNLOAD EBOOKThe torque developed by the interaction of current-carrying coils with the earth's magnetic field can be used as a means of attitude control. The degree to which the attitude of a vehicle can be maintained utilizing this torque depends on the fluctuations of the magnetic field at the satellite as the satellite orbits about the earth. Due to the nature of the torque developed only two vehicle axes can be c ntinuously controlled simultaneously. With the principle described, either a two- or three-coil system can be used to control vehicle attitude about two axes. Intermittent control about three axes can be obtained. (Author).
Author: United States. Superintendent of Documents
Publisher:
Published: 1979
Total Pages: 1250
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Published: 1966
Total Pages: 712
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DOWNLOAD EBOOKAuthor: United States. Congress
Publisher:
Published: 1960
Total Pages: 1564
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DOWNLOAD EBOOKAuthor: United States. National Aeronautics and Space Administration
Publisher:
Published: 1959
Total Pages: 302
ISBN-13:
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