An approach to design of the rudder—drive system taking into account the aeroelastic characteristics of the rudder is proposed. Mathematical models are developed that are used to solve problems of the rudder design parameters selection and the rudder—drive system stability analysis. An example of design of the rudder—drive system of the air-to-air unmanned aerial vehicle is given.
On One Approach to Design of the Rudder-Drive System Taking into Account the Aeroelastic Stability Requirements
Russ. Aeronaut.
Russian Aeronautics ; 63 , 1 ; 75-82
01.01.2020
8 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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