Zobrazeno 1 - 5
of 5
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
Publikováno v:
Russian Aeronautics; Jan2022, Vol. 65 Issue 1, p121-131, 11p
Publikováno v:
Russian Aeronautics; Jul2021, Vol. 64 Issue 3, p488-496, 9p
Publikováno v:
Russian Aeronautics; Oct2016, Vol. 59 Issue 4, p500-506, 7p