The control law of the available energy of the aircraft for automatic go around

Authors

  • В. С. Морозов Національний авіаційний університет

DOI:

https://doi.org/10.18372/2073-4751.2.8948

Keywords:

автоматичний вихід літака на друге коло, закон управління наявною енергією літака, система автоматичного управління

Abstract

This article gives a test results of automatic go around due to the estimation of the aircraft available energy. The automatic go around is considered as spatial maneuver. The control law of the available energy has been designed to provide the acceleration and climb for maneuver of the automatic go around. The presented control law includes current information about bank angle and available energy. The designed control law provides the implementation of the requirement to minimum gradient of climb for go around

References

Морозов С.В. Автоматичний ви-хід літака на друге коло за критерієм ене-ргетичного швидкісного підйому.// Наукові вісті НТУУ “КПІ”. – 2008. – №2(58). – С. 68-74.

Динамика полета/Ефремов А.В., Захарченко В.Ф., Овчаренко В.Н. и др.; под ред. Бюшгенса Г.С. – М.: Машиностроение, 2011. – 776 с.

Руководство по сертификации самолетов транспортной категории в части средств автоматического управления на соответствие требованиям АП-25. Часть 1. –М.: ЛИИ им. М.М. Громова, 1991. – 25 с.

Пахненко В.Л., Трюхан О.Н., Савченков Ю.Г. Особенности практической аэродинамики самолета Ан-124. – К.: КВВАИУ, 1992. – 112 с.

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Published

2015-06-10

How to Cite

Морозов, В. С. (2015). The control law of the available energy of the aircraft for automatic go around. Problems of Informatization and Control, 2(50), 91–97. https://doi.org/10.18372/2073-4751.2.8948

Issue

Vol. 2 No. 50 (2015)

Section

Статті

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