SIMPLE UNIVERSAL NONLINEAR LONGITUDINAL FLIGHT SIMULATION WITH AVOIDING OF STATIC AND DYNAMIC STABILITY DERIVATIVES

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F18%3APU129805" target="_blank" >RIV/00216305:26210/18:PU129805 - isvavai.cz</a>

Výsledek na webu

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DOI - Digital Object Identifier

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Jazyk výsledku

angličtina

Název v původním jazyce

SIMPLE UNIVERSAL NONLINEAR LONGITUDINAL FLIGHT SIMULATION WITH AVOIDING OF STATIC AND DYNAMIC STABILITY DERIVATIVES

Popis výsledku v původním jazyce

This paper shows a method to simulate nonlinear longitudinal flight dynamic of an aircraft in as most direct way as possible. The method is based on physical principles of an analytical flight dynamics. Presented model has a lot of advantages. The model is as simple as possible, non-linearity as stall or thrust dependent on velocity can be included. Static and dynamic stability derivatives are not required but can be computed as an output of the model. The model can be used for various aircraft conceptions. Higher level model, for example, based on flight tests data, can be modified by low-level analytical methods. For example, for modification of horizontal tail area. No special simulation software is necessary.

Název v anglickém jazyce

SIMPLE UNIVERSAL NONLINEAR LONGITUDINAL FLIGHT SIMULATION WITH AVOIDING OF STATIC AND DYNAMIC STABILITY DERIVATIVES

Popis výsledku anglicky

This paper shows a method to simulate nonlinear longitudinal flight dynamic of an aircraft in as most direct way as possible. The method is based on physical principles of an analytical flight dynamics. Presented model has a lot of advantages. The model is as simple as possible, non-linearity as stall or thrust dependent on velocity can be included. Static and dynamic stability derivatives are not required but can be computed as an output of the model. The model can be used for various aircraft conceptions. Higher level model, for example, based on flight tests data, can be modified by low-level analytical methods. For example, for modification of horizontal tail area. No special simulation software is necessary.

Druh

D - Stať ve sborníku

CEP obor

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OECD FORD obor

20304 - Aerospace engineering

Projekt

<a href="/cs/project/LO1202" target="_blank" >LO1202: NETME CENTRE PLUS</a><br>

Návaznosti

P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění

2018

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název statě ve sborníku

13th Research and Education in Aircraft Design Conference

ISBN

978-80-214-5696-9

ISSN

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e-ISSN

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Počet stran výsledku

196

Strana od-do

130-141

Název nakladatele

Neuveden

Místo vydání

neuveden

Místo konání akce

Brno

Datum konání akce

7. 11. 2018

Typ akce podle státní příslušnosti

EUR - Evropská akce

Kód UT WoS článku

000460498600013