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Analytical construction of interception trajectories in atmosphere
Afanas’ev V.A., Degtyarev G.L., Meshchanov A.S.
Methods of Constructing the Neural Network Models of Regulators for Controlling a Dynamic Object with Smooth Monotonous Behavior
Emaletdinova L.Y., Kabirova A.N.
Control of flight vehicles with the adjustable center of mass
Afanas’ev V.A., Degtyarev G.L., Kiselev V.I., Meshchanov A.S.
Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle
Afanas’ev V.A., Degtyarev G.L., Meshchanov A.S.
Roll control of a flight vehicle with the adjustable center of mass
Afanas’ev V.A., Degtyarev G.L., Kiselev V.I., Meshchanov A.S.
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.
Development of a Combined Electric Power Storage Device
Tishkov A.I., Konoplev Y.V., Shevtsov I.V., Yuev A.A.
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.
Control quality improvement for aircraft engine technological manufacturing processes
Lyutov A.G., Ryabov Y.V., Polezin S.A.
Route optimization of the aircraft flight
Averkiev N.F., Vlasov S.A., Salov V.V., Kiselev V.V.
Research on High-Precision Measurement Systems of Modern Aircraft
Shen K., Neusypin K.A., Selezneva M.S., Proletarskii A.V.
Integrated acoustic monitoring system for jet fuel tanks
Borminskii S.A., Parshina A.V., Skvortsov B.V.
An Anthropocentric Approach for Solving the Problem of Optimal Automatic Landing Flare
Trinh V.T., Nguyen N.M., Dang N.T., Nguyen K.A.
The problem of estimating microaccelerations aboard Foton-M4 spacecraft
Anshakov G.P., Belousov A.I., Sedel’nikov A.V.
Approach to implementing hardware-independent automatic control systems of lathes and lathe-milling CNC machines
Martinov G.M., Nezhmetdinov R.A., Kuliev A.U.
Principles of Constructing the Systems of Restriction the Aircraft Critical Parameters
Petunin V.I., Neugodnikova L.M.
Analytical Synthesis of Stabilization Laws for Spacecraft Orbit Attitude Using Information on an Angle and the Full Vector of Angular Velocity
Zubov N.E., Mikrin E.A., Ryabchenko V.N., Sorokin I.V.
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.
A simulator of the aircraft air data system
Efremova E.S.
Synthesis of Stabilization Laws for Lateral Motion of a Maneuverable Aircraft at the Lack of Data on Its Sideslip and Roll Angles
Zubov N.E., Mikrin E.A., Ryabchenko V.N., Sorokin I.V.
On a Problem of Optimal Control of the Laminar Boundary Layer in Supersonic Flows on Constant-Pressure Surfaces
Garaev T.K., Osadchaya D.M.
The aerospace vehicle control characterizing by considerable time delay
Efremov A.V., Tyaglik M.S., Tyaglik A.S., Aleksandrov V.V.
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.
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.
Algorithms of Constructing the Regions of Initial States for Unmanned Winged Gliders
Grumondz V.T., Karpezhnikov E.I., Polishchuk M.A., Polishchuk M.V.
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