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Kiev, Ukraine

Number of publications: 3

Summary: The computational model of additional errors, which occur from interaction of intense shock N-wave with inertial positioning devices of hypersonic aircraft was built. Angles of coincidence for the industrial design of the angular velocity sensor were fitted. A comparative analysis of the experimental data for seminatural conditions for the two cases (gyroscope ON, gyroscope OFF) was made. Conclusions about the possibility of use of the results were made.

Key words: N-wave, hypersonic aircraft, caustic zone, wave coincidence, float gyroscope.


Branch of science: Technical sciences
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