SIMULATION OF AIRCRAFT ABRUPT RESPONSE IN DIRECTIONAL CONTROL

Pavel Anatolievich Desyatnik

doi:10.1615/TsAGISciJ.v41.i4.80

TsAGI Science Journal

Главный редактор: Sergei Leonidovich Chernyshev (open in a new tab)

Ассоциированный редактор: Ivan Vladimirovich Egorov (open in a new tab)

International Executive Editorial Advisors: M. de Gliniasty (open in a new tab) C.W. Kauffman (open in a new tab) Jurgen Quest (open in a new tab) Gu Songfen (open in a new tab) Shinji Suzuki (open in a new tab)

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ISSN Печать: 1948-2590

ISSN Онлайн: 1948-2604

SIMULATION OF AIRCRAFT ABRUPT RESPONSE IN DIRECTIONAL CONTROL

Том 41, Выпуск 4, 2010, pp. 471-480

DOI: 10.1615/TsAGISciJ.v41.i4.80

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Pavel Anatolievich Desyatnik
Central Aerohydrodynamic Institute (TsAGI), 1 Zhukovsky str., Zhukovsky 140180, Moscow region, Russia

Краткое описание

Considered are the problems of on-ground, motion-on simulation of specific forces and angular accelerations arising from aircraft abrupt response (AR) to pilot activity with regard to directional control. A method to simulate specific forces and angular accelerations is developed to predict the AR phenomenon at the first stages of aircraft development. Special attention was paid to the selection of motion system drive algorithms and their parameters with regard to directional AR reproduction. The motion system drive algorithm parameters were selected for different piloting tasks.

Ключевые слова: aircraft handling qualities (HQs), abrupt response (AR), flight simulator, motion system drive algorithms, directional control

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