CRITERION TO SELECT OPTIMUM VALUES OF AIRCRAFT LATERAL STATIC STABILITY MARGIN IN LANDING APPROACH

Pavel Anatolievich Desyatnik

doi:10.1615/TsAGISciJ.v46.i7.50

TsAGI Science Journal

Editor en Jefe: Sergei Leonidovich Chernyshev (open in a new tab)

Editor Asociado: 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)

Publicado 6 números por año

ISSN Imprimir: 1948-2590

ISSN En Línea: 1948-2604

CRITERION TO SELECT OPTIMUM VALUES OF AIRCRAFT LATERAL STATIC STABILITY MARGIN IN LANDING APPROACH

Volumen 46, Edición 7, 2015, pp. 671-686

DOI: 10.1615/TsAGISciJ.v46.i7.50

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

SINOPSIS

The equation of aircraft lateral/directional motion is analyzed and modified to determine generalized parameters critical to developing the handling quality criterion in the directional control axis. An extensive experimental database is collected on the TsAGI PSPK-102 flight simulator to assess the effect of the generalized parameters on the optimum (pilot opinion) values of L_β that determine the best interaction between directional and lateral motion while under pedal control. The derivation of the directional handling quality criterion is presented based on the collected experimental database. The effectiveness of the criterion is demonstrated by its coincidence with the experimental results.

PALABRAS CLAVE: lateral static stability margin, transport aircraft, directional handling qualities criterion, flight simulator

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