Receipt date: 
24.09.2018
Year: 
2018
Journal number: 
УДК: 
681.5
Article File: 
Pages: 
29
37
Abstract: 

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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