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Flight duration, potential and relative efficiency of an electric multicopter
Sverdlov S.
Numerical Analysis of Hovering Main Rotor Aero-Acoustic Characteristics for Ice Detection
Chen X., Zhao Q., Barakos G., Kusyumov A.
The Concept and Definition of Integrated Flight Performance for a Small Remotely Piloted Helicopter
D’yakonov D., Zavalov O., Turkin I.
Development of wireless strain-gauge measurement system for structural tests
Uvarov M., Naumov V.
Control synthesis for an unmanned helicopter with time-delay under uncertain external disturbances
Garkushenko V., Vinogradov S., Barakos G.
Electric Drive with Magnetic Reduction of the Helicopter Main Rotor
Afanas’ev A., Berezov N., Rybushkin N.
Influence of the Air Viscosity on the Induced Power of a Helicopter Main Rotor in Hover and Vertical Takeoff Modes
Shaidakov V., Brusov V.
Improving the noise stability of measuring the altitude and speed parameters aboard a helicopter
Nikitin A., Soldatkin V., Soldatkin V.
Computational modeling of interference between helicopter main and tail rotors based on nonlinear blade vortex model
Ignatkin Y., Makeev P., Shomov A.
Construction and Algorithms of the Onboard System for Measuring the Helicopter Air Data and State of the Atmosphere with a Stationary Receiver, Ion-Mark and Aerometric Measurement Channels
Soldatkin V., Nikitin A., Ariskin E.
Numerical Modeling of Helicopter Main Rotor Behavior near a Small-Scale Helideck by the Vortex Method
Aparinov A., Kritskii B., Setukha A.
Modeling of helicopter flight imitation in the vortex ring state
Toropov M., Stepanov S.
Assessment of Improving Performance of an Imitation Model with Respect to the Real Flight Characteristics of a Helicopter
Ledyankina O., Girfanov A.
Construction and algorithms of a helicopter air data system with aerometric and ion-tagging measurement channels
Soldatkin V., Nikitin A.
On a certain approach to modeling aerodynamics and dynamics of spatial motion of single rotor helicopters
Onushkin Y., Sizov D., Poluyakhtov V., Pidodnya V., Ostrovoi A.
Stability of Decisions in Choosing the Operating Parameter Values of the Gas Turbine Engine in the Helicopter System at the Initial Design Stage
Grigor’ev V., Zagrebel’nyi A.
Analysis and synthesis of the information-controlling system channels to prevent critical operating conditions of the helicopter flight
Kuznetsov O., Soldatkin V.
Composite model of a research flight simulator for a helicopter with the hingeless main rotor
Ledyankina O., Mikhailov S.
Comparative Analysis of Techniques of Modeling Kinematic Relations for Solving Helicopter Motion Equations
Girfanov A.
Influence of the helicopter flight design speed on the selection of working process parameters for GTE
Grigor’ev V., Zagrebel’nyi A.
Numerical modeling of helicopter flight on a prescribed trajectory
Girfanov A., Girfanova R.
Study of the Local Strength of the Main Rotor Torsion Bar under the Action of Flight and Test Bench Loads
Mitryaikin V., Shuvalov V.
Comprehensive approach to mathematical modeling and helicopter flight task optimization
Onushkin Y., Sizov D., Poluyakhtov V.
Method of determining the maximum permissible values for diagnostic signs of helicopter transmission units operational status
Nedel’ko D.
Investigation of Modeling Possibility for Lagging of a Helicopter Operating in Transient Flight Regimes
Girfanov A., Ledyankina O., Gimadiev R.
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