Dynamic Model of Aircraft Landing

Transport and Aerospace Engineering 2016
Artūrs Suharevs, Pjotrs Trifonovs-Bogdanovs, Vladimirs Šestakovs, Konstantin Mamay

Manuscript presents a research method that will be used in the development process of avionics equipment. A special device predicting braking and take-off distances will help pilots and provide a complex increase of flight safety and decrease of some types of charges.

Keywords
Aircraft dynamic model, braking, landing, runway run distance, rolling resistance force.
DOI
10.1515/tae-2016-0005
Hyperlink
https://content.sciendo.com/view/journals/tae/3/1/article-p38.xml

Suharevs, A., Trifonovs-Bogdanovs, P., Šestakovs, V., Mamay, K. Dynamic Model of Aircraft Landing. Transport and Aerospace Engineering, 2016, Vol.3, pp.38-43. ISSN 2255-968X. e-ISSN 2255-9876. Available from: doi:10.1515/tae-2016-0005

Publication language
English (en)