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Документ Рациональный синтез аэродинамической компоновки органов управления креном маневренного самолета(НТУ "ХПИ", 2012) Ковтонюк, И. Б.This research paper describes rational synthesis method of aerodynamic arrangement of maneuverable aircraft roll controls. It allows to choose rational way which provides high speed of aircraft roll at basic flight reference from alternative variants of aerodynamic arrangement of aircraft lateral controlsДокумент Статистический показатель рациональности аэродинамической компоновки органов поперечного управления самолета(НТУ "ХПИ", 2011) Ковтонюк, И. Б.Offered static index of rationality of aerodynamic arrangement of lateral controls management of airplane, which will allow to estimate influence of structurally layout decisions which are accepted on the early stages of planning, on efficiency of lateral control of airplane.Документ Обоснование требований к характеристикам маневренности, устойчивости и управляемости истребителей при перехвате малоскоростных целей(НТУ "ХПИ", 2010) Анипко, О. Б.; Ковтонюк, И. Б.Offered approach to the ground requirements to characteristics of maneuverability, stability and controllability of interceptors, at the intercept of littlespeed aims. Approach includes for itself the stages of analysis of interceptor as a difficult technical system, forming of rational parameters and characteristics of maneuverability, stability and controllability, and final stage of forming actually of requirements to characteristics of maneuve rability, stability and controllability of interceptor.Документ Потребное управление летательным аппаратом с учетом отклонения траектории полета от заданной(НТУ "ХПИ", 2009) Ковтонюк, И. Б.; Анипко, О. Б.Offered approach to determination of required control of LA, which takes into account deviation of trajectory of flight of LA from setting. A required control is considered for the task of intercept of air purpose which moves.Документ Потребное управление при синтезе средств обеспечения устойчивости и управляемости летательного аппарата(НТУ "ХПИ", 2009) Ковтонюк, И. Б.; Анипко, О. Б.The method of synthesis of devices which provide stability and controllability of aircraft is offered in this work at the level of conception, allowing from all of aggregate of alternative va riants to choose such, which provide implementation of the set terms of flight and required level of pilotage properties taking into account present limits on the ranges of rejection of aircraft control.