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The fiber-optical gauge of pressure for the control system of engine BPLA
Leonovich G.I., Matjunin S.A., Kilejnov Y.U., Livochkina H.A., Solovjov V.I.
Optimization of the parameters of a ground speed meter of low-flying aircraft based on the application of the theory of optimal filtration
Ivanov M.E., Yezerskiy V.V.
Concept of multilevel adaptation of integrated navigation systems of small spacecraft
Fominov I.V.
Mathematical model of the inline sensor based on matrix photodetector
Kornilin D.V.
Single-coil eddy-current transducers for measuring mechanical parameters
Borovik S.Y., Sekisov Y.N.
Dynamics of the hydromechanical system of a production machine with an adaptive tool-feeding drive
Sidorenko V.S., Poleshkin M.S., Rakulenko S.V.
Electrization of the surface of low-orbiting small spacecraft “AIST”
Syomkin N.D., Bragin V.V., Piyakov A.V., Telegin A.M., Ryazanov D.M., Matviets M.G.
Use of approximative analysis outcome of experiment in problem of diagnostics technical conditions of hydraulic systems
Malchikov K.Y., Logvinov L.M., Kovalev M.A.
On-board algorithm for SamSat-218D nanosatellite orientation and stabilization system
Kramlikh A.V., Melnik M.E.
Differential bynary optical-mechanical sensors for automated management and control systems
Korban D.V.
Analysis of determinate error of an optoelectronic angular shift sensor on multicomponent optronic structures
Stepanov M.V., Matyunin S.A.
Pilot study of frequency characteristics of an acoustic probe for measuring pressure pulsations in the gas turbine engine inlet device
Ivanenko V.N., Alexandrova T.G., Dyagileva E.C., Gimadiyev A.G., Bystrov N.D.
Autocalibration measuring channel on the input channel conversion electric values
Vilop L.E.
Criteria of discrete phase control of blade working condition and their feasibility in systems of turbine driven set automatic control
Danilin A.I., Tchernyavsky A.Z.
Indirect determination of the presence of vibration combustion in combustion chambers of turbine engines by a three-channel sensor for measuring movement
Limanova N.I., Yudin P.Y., Limanov I.A.
Measurements of pulse pressures within the volume of a melt in terms of intense impulse interferences
Yusupov R.Y., Kostryukov E.E.
The devices for the diagnosis and control of turbine blades deformative condition during operation
Danilin A.I., Chernyavskiy A.G., Kapustin A.S.
Fiber-optical pressure transducer for the UA engine control system
Leonovich G.I., Matyunin S.A., Glushkov A.I., Livochkina N.A., Solovyov V.I.
Small-sized two-coordinate sensor of the Sun’s angular position with enlarged field of view
Dyuldin R.S., Blinov V.D.
Study of flow characteristics in straight-flow combustion chamber with sudden expansion
Egorov A.G., Zotkin V.I., Ivanin S.V.
Bringing spacecraft into solar-oriented attitude by the measurements of a single-axis angular-rate sensor and an optical solar sensor
Shipov M.G., Steklova A.A., Davydov A.A.
Research of flame distribution speed, width of the zone and intensity of chemical reactions of combustion in the spark-ignition engine
Bobrovskiy I.N., Shaykin A.P., Brizgalov A.A., Sukhov S.A.
Authenticity of the vibration tests. Diagnosis and prediction of fatigue failure
Ovchinnikov I.N., Ermishkin V.A.
Analysis of the error of non-linearity of positional characteristics of a displacement transducer on multicomponent optronic structures
Matyunin S.A., Stepanov M.V.
Experimental research of staff LTRE with hypergolic propellant under impulse engaging conditions
Shustov S.A.
Method of parametric optimization of each component of adaptive compensatng inertial sensors operating in a self-oscilation mode
Fominov I.V.
Development of a small-sized acoustic probe for the measurement of pressure pulsations in the gasdynamic duct of gas turbine engines
Gimadiyev A.G., Bystrov N.D., Ilyinsky S.A.
Converting sensor capacity into standardized signals with structural and time redundancy
Artamonov P.I.
1 - 28 of 28 Items

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