DocumentCode
3314922
Title
Meter of gyrodines moments
Author
Gormakov, N. ; Shpak, N.V.
Author_Institution
Tomsk Polytech. Inst., Russia
fYear
2003
fDate
7-11 April 2003
Firstpage
89
Lastpage
91
Abstract
Currently the control of the orbit probes and the Earth´s artificial satellites orientation is carried out by means of active systems, the executive units of which are the gyrodines. The accuracy of the orientation to considerable degree depends on the quality of the controlling moments developed by the gyrodines. This paper describes a gyrodine design to provide for the measurement of the constant and alternating moments within the required range with the specified accuracy.
Keywords
artificial satellites; position control; alternating moments; artificial satellites orientation; compensation principle; constant moments; controlling moments; gyrodine moments; moment meter; orbit probes; Bridge circuits; Detectors; Engines; Frequency; Low-noise amplifiers; Narrowband; Noise level; Phase detection; Phase noise; Voltage;
fLanguage
English
Publisher
ieee
Conference_Titel
Modern Techniques and Technologies, 2003. MTT 2003. Proceedings of the 9th International Scientific and Practical Conference of Students, Post-graduates and Young Scientists
Print_ISBN
0-7803-7669-2
Type
conf
DOI
10.1109/SPCMTT.2003.1438144
Filename
1438144
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