Zobrazeno 1 - 1
of 1
pro vyhledávání: '"aerodynamic inteceptor"'
Publikováno v:
Scientific Technical Review, Vol 67, Iss 2, Pp 37-46 (2017)
The excessive roll of air-launched missiles is a result of disturbances during the flight due to airframe misalignment, asymmetric control in pitch and yaw planes, atmospheric disturbances or large torque disturbances in the vicinity of aircraft. In
Externí odkaz:
https://doaj.org/article/e644e48f961d4ed78cc4b47c9abae932
