Study of Systems Using Inertia Wheels for Precise Attitude Control of a Satellite
Author : John S. White
Publisher :
Page : 78 pages
File Size : 34,92 MB
Release : 1961
Category : Satellites
ISBN :
Author : John S. White
Publisher :
Page : 78 pages
File Size : 34,92 MB
Release : 1961
Category : Satellites
ISBN :
Author : John S. White
Publisher :
Page : 71 pages
File Size : 38,44 MB
Release : 1961
Category :
ISBN :
Author : John S. White
Publisher :
Page : 44 pages
File Size : 47,8 MB
Release : 1961
Category : Satellites
ISBN :
Author : James J. Adams
Publisher :
Page : 22 pages
File Size : 24,38 MB
Release : 1963
Category : Artificial satellites
ISBN :
Author :
Publisher :
Page : 468 pages
File Size : 22,84 MB
Release : 1966
Category :
ISBN :
Author : Stuart C. Brown
Publisher :
Page : 68 pages
File Size : 14,66 MB
Release : 1961
Category :
ISBN :
Author :
Publisher :
Page : 1878 pages
File Size : 12,91 MB
Release : 1961
Category : Government publications
ISBN :
Author : John S. White (writer on artificial satellites.)
Publisher :
Page : 42 pages
File Size : 46,95 MB
Release : 1961
Category : Artificial satellites
ISBN :
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).
Author : United States. Superintendent of Documents
Publisher :
Page : 1250 pages
File Size : 34,5 MB
Release : 1979
Category : United States
ISBN :
Author :
Publisher :
Page : 712 pages
File Size : 26,46 MB
Release : 1966
Category : Mechanics, Applied
ISBN :