Critical Flight Conditions at High Angles of Attack, Related to Loss of Control in Lateral Motion

Critical Flight Conditions at High Angles of Attack, Related to Loss of Control in Lateral Motion

El documento trata sobre el desarrollo de algoritmos para el diagns̤tico de přdida de carga y la proteccin̤ de los aviones para que no se encuentren con un giro posterior a la přdida de carga y para que no entren en modo de giro. Resume los resultados de la teora̕ lineal de la přdida de control d...

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Detaylı Bibliyografya
Diğer Yazarlar: Akhrameev V.I, Glazkov A.A, Shibaev V.M, Shoulepov D.V, University of Defence
Materyal Türü: Kitap
Dil:İngilizce
Konular:
Sistemas de control digital
Aeronave
Aerodinm̀ica
Digital control systems
Aircraft
Aerodynamics
Dinm̀ica del avin̤
altos ǹgulos de ataque
přdida de control del avin̤
modos de vuelo crt̕icos
inmunidad a přdida y giro
sistema de advertencia
automatizacin̤ del control del avin̤.
Airplane dynamics
high angles of attack
airplane loss-of-control
critical flight modes
stall and spin immunity
warning system
airplane control automation.
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Critical Flight Conditions at High Angles of Attack, Related to Loss of Control in Lateral Motion

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