The mathematical model of aerometric devices errors on the basis of different information integration according to flight recorders

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UDCΒ 629.7Β BBKΒ 39.56

ShomankovΒ D.Β A.Β 

The mathematical model presented in the article is based on the integration of different flight information recorded by the means of objective control and can be used in the systems of optimized evaluation of high-speed flight parameters or technical control of aerometric measuring devices.

Keywords: integration, correlation function, generating filter, errors, optimized evaluation, control, technical condition

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