Zobrazeno 1 - 1
of 1
pro vyhledávání: '"G. V. Kondrashev"'
Publikováno v:
Russian Aeronautics (Iz VUZ). 59:331-337
Theoretical and experimental methods of investigating the performance of an electric actuator of maneuverable unmanned aerial vehicle (UAV) is considered in order to solve the aeroelasticity tasks. Models of the stability analysis for the rudder–ac