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Small-Size Automatic System for the Controllable Launch of Nanosatellites on a Desired Trajectory
Filonin O.V., Belokonov I.V., Gimranov Z.I.
Design Features and Efficiency Analysis of the Aircraft Complex Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V.M.
Research on High-Precision Measurement Systems of Modern Aircraft
Shen K., Neusypin K.A., Selezneva M.S., Proletarskii A.V.
A simulator of the aircraft air data system
Efremova E.S.
Development of the Wireless Control System for Shape of Large Transformed Structures Using Precision Drives
Evstigneeva E.I., Lekanov A.V., Matveev S.A., Shirshov A.D., Yakovenko N.G.
Analyzing and Ensuring the Dynamic Accuracy of the Aircraft Air Data System with a Fixed Flush-Mounted Flow Receiver
Soldatkin V.M., Soldatkin V.V., Nikitin A.V., Kornilov V.Y.
Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System
Kornev A.V., Sereda V.A., Migalin K.V.
Design of gating systems in production of gas turbine engine blades
Smykov A.F., Moiseev V.S., Chumadin A.S.
Methods for measuring the geometric parameters of products by the laser coordinate measuring system in modern mechanical production
Lyudogovskii P.L., Komkova M.A.
Concept of monitoring for thermostressed state and service life of aircraft gas turbine engine blades
Kulikov G.G., Trushin V.A., Abdulnagimov A.I., Ganeev A.A.
Developing the Mathematical Model of a Pilot in a Control Manual Preview Tracking Task
Efremov A.V., Tyaglik M.S., Tyaglik A.S., Irgaleev I.K.
Advanced Pulsed Plasma Thrusters and Their Application as a Part of Small Spacecraft Propulsion Systems
Bogatyi A.V., El’nikov R.V., Nazarenko I.P., Popov G.A., Semenikhin S.A.
Loads and Stress-Strain State of Gas Turbine Engine Bearing Cages
Murashkin V.V., Klebanov Y.M., Danilchenko A.I., Adeyanov I.E.
Physical modeling of electromagnetic interferences in the unmanned aerial vehicle in the case of high-voltage transmission line impact
Nuriev M.G., Gizatullin Z.M., Gizatullin R.M.
Improving the noise stability of measuring the altitude and speed parameters aboard a helicopter
Nikitin A.V., Soldatkin V.V., Soldatkin V.M.
Development of the design scheme of cooling for a nozzle vane of high pressure turbine of gas turbine engine
Vikulin A.V., Yaroslavtsev N.L., Chesnova V.A.
Definition of the Generation Instants in Time of the Running Shaft Resonant Flexural Vibrations by Means of Indicator Function of the Number of States of Dynamic System
Tukmakov A.L., Tukmakova N.A.
Solving the Autonomous Initial Navigation Task for Strapdown Inertial Navigation System on the Perturbed Basis Using Rodriguez—Hamilton Parameters
Sokolov S.V., Pogorelov V.A., Shatalov A.B.
Development of Algorithms for Integration and Reconfiguration of the Flight Control System and Interfaces
Efremov A.V., Tyaglik M.S., Tyaglik A.S., Irgaleev I.K.
On a Problem of Optimal Control of the Laminar Boundary Layer in Supersonic Flows on Constant-Pressure Surfaces
Garaev T.K., Osadchaya D.M.
Analysis and synthesis of the information-controlling system channels to prevent critical operating conditions of the helicopter flight
Kuznetsov O.I., Soldatkin V.M.
Spatial vibration protection in a turbopump of hydrogen rocket engines
Belousov A.I., Ponomarev Y.K.
About Optimal Reception of Pseudorandom Signals of Nonlinear Dynamic Systems
Nasyrov I.K., Andreev V.V.
Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters
Petunin V.I., Neugodnikova L.M.
Efficiency Estimation of Electrothermal Thrusters Use in the Control System of the Technological Spacecraft Motion
Anshakov G.P., Belousov A.I., Sedel’nikov A.V., Gorozhankina A.S.
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