Study of Systems Using Inertia Wheels for Precise Attitude Control of a Satellite PDF Download
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Author: John S. White
Publisher:
ISBN:
Category : Satellites
Languages : en
Pages : 78
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Book Description
Author: John S. White
Publisher:
ISBN:
Category : Satellites
Languages : en
Pages : 78
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Book Description
Author: John S. White
Publisher:
ISBN:
Category : Satellites
Languages : en
Pages : 44
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 864
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Author: John S. White (writer on artificial satellites.)
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 42
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Book Description
The 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).
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Category : Government publications
Languages : en
Pages : 1878
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Author: Defense Documentation Center (U.S.)
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ISBN:
Category : Military art and science
Languages : en
Pages : 1746
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Author: Frederick G. Edwards
Publisher:
ISBN:
Category : Artificial satellites
Languages : en
Pages : 60
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Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 712
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Author: United States. Superintendent of Documents
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ISBN:
Category : United States
Languages : en
Pages : 1284
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 610
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