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Reducing energy consumption of vertical take-off and landing unmanned aerial vehicle using hybrid technical solutions
Lukyanov O.E., Hoang V.H., Komarov V.A., Nazarov D.V., Kurkin E.I., Quijada Pioquinto J.G., Chertykovtseva V.O.
Mathematical model of a generalized quadcopter kinematic scheme and its software implementation
Zelenskiy V.A., Kovalev M.A., Ovakimyan D.N., Kirillov V.S.
Algoritms for determining the attitude position of an unmanned aerial vehicle relative to the landing platform by using computer vision
Gainutdinova T.Y., Novikova S.V., Gainutdinov V.G., Trusfus M.V., Litvin V.M.
Selection of aerodynamic characteristics and engine parameters of a maneuverable aircraft under epistemic uncertainty
Veresnikov G.S., Ogorodnikov O.V.
Experimental analysis of instability and self-oscillations in an electrohydraulic servo drive
Petrov P.V., Sunarchin R.A., Mashkov M.A., Krivosheev N.S.
Automation of the process of testing on-board systems of unmanned aerial vehicles
Kirillov A.V., Sitnikov V.V., Tuchin A.L.
Main approaches and features of the design of aircraft hydro-mechanical control systems
Petrov P.V., Tselischev V.A., Kuderko D.A.
Development of ordinary harness for aircraft onboard cable networks
Koptev A.N., Myasnikov A.Y.
Metrological analysis of a device rof nondestructive control of flight vehicle fuel tank current conductive coatings
Samsonov A.S., Blinov D.I., Skvortsov B.V., Zhivonosnovskaya D.M.
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.
Optimal control of the angle of attack of a hypersonic flight vehicle
Bebyakov A.A.
Application of dynamic programming for path planning for observation of mobile ground targets in the controlled area
Lebedev G.N., Efimov A.V.
Influence of turbulence models on calculated values of aircraft aerodynamic properties
Elisov N.A., Ishkov S.A., Shakhov V.G.
Research of a sleeve connection of the aircraft pipeline under the influence of dynamic loading
Agafonov V.M., Pykhalov A.A.
The main trends of aviation science development
Alyoshin B.S., Chernyshev S.L.
Ensuring permissible level of gas turbine dynamic loading in operation by means of standard engine control devices
Chervonyuk V.V., Korovin B.B.
Optimization of space vehicle trans-atmospheric motion by using the method of sequential linearization
Balakin V.L., Ishkov S.A., Khramov A.A.
Multicriterial choice of the best variant of the pulse detonation engine design for aircraft angular stabilization and orientation systems
Safronov V.V., Porshnev V.A., Zhebrakov A.S.
Adjustment of the pneumatic drive of a ground catapult to the permanent law of tractive force
Sereda V.A.
Determination of the optimal parameters and engine layout for a strike unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Agaverdyev S.V.
Engines for domestic drones: past, present and future
Cherkasov A.N., Legkonogikh D.S., Zinenkov Y.V., Panov S.Y.
Complex approach to aerodynamic design of inlet ducts with submerged vortex-free air intakes
Kornev A.V., Boychuk I.P.
Reduction of circumferential variation in the final stage of IPC
Popov G.M., Mamedov A.C., Smirnova Y.D.
Selection of the optimum configuration and calculation studies of the parameters of a cryogenic propulsion system for an unmanned aerial vehicle
Tremkina O.V., Uglanov D.A., Urlapkin V.V., Korneev S.S., Komisar Y.V.
Estimating the efficiency of a bypass turbojet engine on the basis of a serial gas generator as a part of the power plant of a high-altitude unmanned aerial vehicle
Zinenkov Y.V., Lukovnikov A.V., Popov A.V., Nechaev V.N.
Prospective lines of improving the process of evaluating the technical condition of aircraft hydraulic system working fluid
Koptev A.N., Gareyev A.M., Popelnyuk I.A.
Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria
Tkachenko A.Y., Kuzmichev V.S.
Laser-scanning rangefinder fixed on a gimbal with two degrees of freedom
Zelenskiy V.A., Kapalin M.V.
Backstepping synthesis of the height control system of an unmanned aerial vehicle
Akhramovich S.A., Barinov A.V., Malyshev V.V., Starkov A.V.
Efficiency of terminal control in the trans-atmospheric first stage of an aerospace system under atmospheric and aerodynamic disturbances
Balakin V.L., Kovalyov A.V., Krikunov M.M.
Problems and prospect of microgasturbines development for unmanned aerial vehicle propulsion
Zhdanov I.A., Staudacher S., Falaleev S.V.
Analysis of basic concepts of advanced engines for supersonic civil aircraft on the basis of foreign designers’ experience
Alendar A.D., Grunin A.N., Siluyanova M.V.
Photoelectric converters in the power supply system of an atmospheric pseudo satellite
Kovalyov M.A., Zelensky V.A., Nazarov A.A., Оvаkimyan D.N., Мirzoev R.M.
Terminal control of aerospace system subhypersonic first stage
Balakin V.L., Kovalyov A.V.
Use of the mathematical tool of hypervector ranging for selection energy-power plant of flight vehicles
Safronov V.V., Zhebrakov A.S.
Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel
Kolesnikov A.S., Grasko T.V., Raznoschikov V.V.
Optimizing a vehicle trans-atmospheric motion using Pontryagin’s maximum principle
Balakin V.L., Ishkov S.A., Khramov A.A.
Influence of the suspension system on the accuracy of the aircraft modal testing results
Berns V.A., Dolgopolov A.V., Zhukov E.P., Marinin D.A.
Command control of hypersonic aircraft angle of attack during acceleration and climb
Kotchyan A.G.
1 - 39 of 39 Items

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