ISSN 0021-3454 (print version)
ISSN 2500-0381 (online version)
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Author
int(20197)

Soldatkin Vyacheslav V.

Work place: A. N. Tupolev Kazan National Research Technical University, Department of Devices and InformationMeasuring Systems
Post: Associate Professor
Degree: Dr. Sci
E-mail: w-soldatkin@mail.ru
Nikitin Alexander V. , Soldatkin Vladimir М., Soldatkin Vyacheslav V. SYSTEM FOR MEASURING HELICOPTER MOVEMENT PARAMETERS UNDER DISTURBANCES OF THE VORTEX COLUMN OF THE ROTOR
The article was published in issue10(61) за 2018
Nikitin Alexander V. , Soldatkin Vyacheslav V. , Soldatkin Vladimir М. STATIC ACCURACY ANALYSIS OF AIR SIGNAL SYSTEM OF AIRCRAFT WITH A FIXED NON-PROTRUDING RECEIVER OF INCOMING AIR FLOW
The article was published in issue8(62) за 2019
Soldatkin Vyacheslav V. , Soldatkin Vladimir М. CONSTRUCTION, MODELS, AND SIGNALS PROCESSING OF MULTIFUNCTIONAL RECEIVER IN AIRCRAFT AEROMETRIC SYSTEMS
The article was published in issue7(64) за 2021
Elena S. Efremova, Nikitin Alexander V. , Soldatkin Vyacheslav V. , Soldatkin Vladimir М. THEORETICAL BASES OF DEVELOPMENT AND RESEARCH OF ELECTRONIC SENSOR OF SMALL-SIZED AIRCRAFT SPEED VECTOR PARAMETERS
The article was published in issue9(64) за 2021
Aleхandеr A. Pavlovskiy, Soldatkin Vyacheslav V. , Soldatkin Vladimir М. ESTIMATION OF THE SPREAD OF AERODYNAMIC CHARACTERISTICS IN MULTIFUNCTIONAL AIR PRESSURE RECEIVER
The article was published in issue6(65) за 2022
Elena S. Efremova, Miftakhov Bylat I. , Soldatkin Vyacheslav V. , Soldatkin Vladimir М. METHODOLOGICAL ERRORS OF AN ELECTRONIC SENSOR OF AIRCRAFT AIRSPEED VECTOR PARAMETERS
The article was published in issue6(66) за 2023
Soldatkin Vladimir М., Soldatkin Vyacheslav V. , Elena S. Efremova, Nikitin Alexander V. CONSTRUCTION, MODELING OF SIGNAL FORMATION AND PROCESSING FOR AIR PARAMETERS MEASURING SYSTEM WITH THE INTEGRATED FUSELAGE FLOW RECEIVER
The article was published in issue2(67) за 2024
Elena S. Efremova, Soldatkin Vyacheslav V. , Soldatkin Vladimir М. CHANNEL ERROR OF THE AIR MOTION PARAMETERS MEASUREMENT SYSTEM FOR AIRCRAFT WITH AN INTEGRATED FUSELAGE FLOW RECEIVER
The article was published in issue10(67) за 2024