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Hardware reconfiguration algorithm in multiprocessor systems of integrated modular avionics
Degtyarev A.R., Kiselev S.K.
The aerospace vehicle control characterizing by considerable time delay
Efremov A.V., Tyaglik M.S., Tyaglik A.S., Aleksandrov V.V.
Robust Controller Synthesis for Airborne Electro-Optical Device Line-of-Sight Stabilization System with Saturating Actuators
Degtyarev G.L., Faizutdinov R.N., Spiridonov I.O., Gubaidullin S.I., Kudryavtsev I.D.
Methods of Constructing the Neural Network Models of Regulators for Controlling a Dynamic Object with Smooth Monotonous Behavior
Emaletdinova L.Y., Kabirova A.N.
Multiobjective Robust Controller Synthesis for Airborne Electro-Optical Device Line-of-Sight Stabilization System
Degtyarev G.L., Faizutdinov R.N., Spiridonov I.O.
Determination of Slag Retention Ability of Gating Systems
Izotov V.A., Serebryakov S.P., Shatul’skii A.A.
Methodological foundations and areas for improvement of the aircraft design process
Liseitsev N.K., Matveenko A.M., Ovcharenko V.N.
Synthesis of control laws for aircraft lateral motion at the lack of data on the slip angle: Analytical solution
Zubov N.E., Mikrin E.A., Ryabchenko V.N., Fomichev A.V.
Fuzzy logic rule as a method for making a design decision in rocketry development
Zezin V.G., Reshetnikov M.I.
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.
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