Errors of two-stage gyro in semi-natural conditions of hypersonic flight

1Shybetskiy, VYu.
1National Technical University of Ukraine “Kyiv Polytechnic Institute”, Kyiv, Ukraine
Kosm. nauka tehnol. 2014, 20 ;(2):52-54
https://doi.org/10.15407/knit2014.02.052
Section: Spacecraft Dynamics and Control
Publication Language: Ukrainian
Abstract: 

We present our results of semi-natural bench tests of uniform angular velocity sensor in the ultrasound beam which occurs in the operation of a hypersonic aircraft. It is proved that there are additional areas of caustic in wave pattern space.

Keywords: angular velocity gyro sensor, hypersonic aircraft
References: 

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