Zobrazeno 1 - 2
of 2
pro vyhledávání: '"A. V. Ostrovoi"'
Publikováno v:
Russian Aeronautics. 64:488-496
Publikováno v:
Russian Aeronautics. 59:500-506
An approach that can be used for modeling the situation of unanticipated yaw is presented. A software is developed that allows us to obtain the helicopter equilibrium attitude at an arbitrary speed and consider the helicopter dynamics under influence