Corrected gyrocompass synthesis as a system with changeable structure for aviation gravimetric system with piezoelectric gravimeter
EN Bezvesilnaya, AH Tkachuk - Aviation, 2014 - Taylor & Francis
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) under the previously mentioned switching is
shown. On the basis of given requirements, we chose the parameters which provide the
device with a switching-back into the gyrocompass mode under any initial gyrocompass …
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) under the previously mentioned switching is
shown. On the basis of given requirements, we chose the parameters which provide the
device with a switching-back into the gyrocompass mode under any initial gyrocompass …
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