Дата поступления: 
24.09.2018
Год: 
2018
Номер журнала (Том): 
УДК: 
681.5
Файл статьи: 
Страницы: 
29
37
Аннотация: 

The article deals with the method of synthesis of algorithms of nonlinear control systems of rotational motion of the aircraft by OZD, the senior derivatives of angular velocities, the analysis of the properties of its own rotational motion described by the dynamic equations of Euler, the conditions of stability of the spiral motion

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