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| A.V. Bykovsky, S.А. Chernikov |
CALIBRATION OF THE PLATFORM SYSTEM IN THE ALIGNMENT MODE
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| V.P. Podchezertsev, Tang Xingyuan, Qin Zihao |
COMPONENTS OF MODEL OF DRIFT DYNAMICALLY TUNED GYRO
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| Yu.G. Egorov, S.А. Chernikov, E.A. Popov |
SYNTHESIS OF THE ACCELEROMETERS TRIAD CALIBRATION PROCESS ON THREE-AXIS DYNAMIC STAND MODEL
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| Yu.G. Egorov, S.А. Chernikov, E.A. Popov |
SYNTHESIS OF THE RATE GYRO TRIAD CALIBRATION PROCESS ON THREE-AXIS DYNAMIC STAND MODEL
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| A.V. Grabik, A.P. Karpenko, A.V. Nekrasov, A.G. Trofimov, A.S. Chernyshev |
PREDICTION OF FUEL CONSUMPTION BY MI-8 HELICOPTER WITH USE OF MODULAR NEURAL NETWORK
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| N.A. Abyshev, S.V. Andreev, A.V. Klyuchnikov |
FEATURES OF A STAND FOR DYAGNOSTICS THE MASS-INERTIA CH ARACTERISTICS OF FLYING MACHINES
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| A.V. Bykov, G.V. Kondrashev, S.G. Parafes, I.K. Turkin |
RESEARCH EXPERIENCE OF ELECTRICAL DRIVES CHARACTERISTICS OF UNMANNED AERIAL VEHICLE BY MEANS OF ELECTROMECHANICAL SIMULATION OF AERODYNAMIC FORCES
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| F.A. Gizatullin, R.M. Salikhov, A.Yu. Barabanov, A.R. Salikhova |
STABILITY OF THE ELECTRIC ARC PROCESS, CHARACTERISTIC OF PLASMA IGNITION SYSTEM FOR GAS TURBINE ENGINES
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| O.V. Phylonin, I.V. Belokonov, Z.G. Gimranov |
MICROPROCESSOR MAGNITOINDUKCIONNAYA SYSTEM FOR START MICRO AND NANOSATELLITES ON GIVEN ORBITS
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