Neural Model of the Aircraft Landing Phase
Journal Title: Archives of Transport - Year 2012, Vol 24, Issue 2
Abstract
The article deals with mathematical modeling of the aircraft landing phase using artificial neural networks. The network was determined based on the data recorded by an aircraft’s quick access recorder. Networks were developed for each flight under review, which resulted from the different durations of this flight phase. It presents the accuracy results of representation across a flight simulation network. It was analyzed how the structure of the neural network affects the quantitative and qualitative accuracy of the actual flight representation. The determined networks will provide a basis for working out a model, among others, for simulation tests of air traffic and flight evaluation. General conclusions about neural networks and basic ones regarding their practical use were formulated.
Authors and Affiliations
Anna Stelmach
Keywords
Related Articles
- EP ID EP70052
- DOI 10.2478/v10174-012-0015-3
- Views 124
- Downloads 0
Safety Management of Complex Airborne and Seaborne Technical Objects
The paper presents some information on a concept of the safety management method of the complex airborne and seaborne technical objects. First of all the differences in safety management in both the seaborne transportati...
Development of a statistically-based methodology for analyzing automatic safety treatments at isolated high-speed signalized intersections
Crashes at isolated rural intersections, particularly those involving vehicles traveling perpendicularly to each other, are especially dangerous due to the high speeds involved. Consequently, transportation agencies are...
The Method of the Evaluation of Transport Systems Operation Safety
Transport safety is the primary standard in the functioning of transport systems. Most of all, it is true in the case of passenger transport systems. This article introduces classification of transport systems into land...
A New Concept of Dual Fuelled SI Engines Run on Gasoline and Alcohol
The paper discusses tests results of dual-fuel spark ignition engine with multipoint injection of alcohol and gasoline, injected in area of inlet valve. Fuelling of the engine was accomplished via prototype inlet system...
THE INF-SUP CONDITION TESTS FOR SHELL/PLATE FINITE ELEMENTS
Development of high-performance finite elements for thick, moderately thick, as well as thin shells and plates, was one of the active areas of the finite element technology for 40 years, followed by hundreds of publicati...