Corrected gyrocompass synthesis as a system with changeable structure for aviation gravimetric system with piezoelectric gravimeter
The present article introduces the development of a corrected gyrocompass with an automatic switch of the gyrocompass into the gyroazimuth mode. The issues of multi-criterion synthesis of the gyrocompass control loop have been studied. The necessity of temporary delay input (with selected values) un...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
Vilnius Gediminas Technical University
2014-10-01
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Series: | Aviation |
Subjects: | |
Online Access: | http://journals.vgtu.lt/index.php/Aviation/article/view/2941 |