Aircraft fly en route under concurrent event situations (conflicting situations), which occur when they operate in the same airspace but are too close to each other in the same time frame. Hence, the safe horizontal distance between them is not less than the standard 5 nm. Free route airspace is such a concept, where such concurrent events need to be resolved when the location and number of such event “hotspots” are random in comparison with fixed route (conventional) airspace. This paper proposes two approaches to solving the traffic conflict in the sector by performing horizontal resolution maneuvers. The first of them uses the Dubins trajectory, while the second one uses a three-fold change of heading (3HC) method (for two types of angles). Apart from maintaining safe separation, we compared them, taking as a criterion the extension of the flight path of aircraft involved in the conflict, as the length of the flight is the primary factor determining flight time/delays and the increase in fuel consumption and greenhouse gas emissions. There may be other algorithms depending on the different data that can be identified through further research.
A dynamic aircraft system conflict (concurrent event) situation exists when a time with a loss (-es) of separation (LOS) in their true or predicted trajectories is determined. Regional air traffic management (ATM) programs aim to make ATM safer and more efficient through a higher level of automation for such processes as dynamic aircraft systems concurrent events detection and, consequently, resolution. Therefore, wind and aircraft speed uncertainty parameters should be properly addressed. This paper offers an approach to a dynamic aircraft system flying under a certain concurrent event situation and demonstrates situation stochastic distribution results (output) based on determined wind speed values (while wind direction angles and the dynamic aircraft system speed values are random). Based on these facts, the stochastic dynamic aircraft system conflict distribution information under determined and random parameters might be retrieved at any specific (preferred) time moment. The observations of this study disclosed that such stochastic output data might have a certain impact on safety matters (potential “domino effect” conflicts on a horizontal plane) and on the efficiency (i.e., flight distance which eventually is a determinant of flight time, fuel costs, delays, emissions, monitoring, etc.).
EUROCONTROL aims at improving the design and use of the European routes. Inefficiencies in the design of airspace and use of the air route network are considered to be a major causal factor of flight inefficiencies in Europe. The European ATM system is the sum total of a large number of separate Air Navigation Service Providers (ANSP) whereas the US system is operated by a single ANSP. Airspace fragmentation following National Borders makes flight routes inefficient due to non requested air routes, flight time, excessive fuel burn, CO and NOx emissions. That is the reason why airspace and the fixed route network should be reorganised to satisfy airspace operator needs and maintain required safety levels.The focus of the paper is to show the differences between planned flights and actual trajectories in terms of flight distance, duration and fuel burn. In connection with this, an overview of these indicators in Europe and the USA was made. EUROCONTROL siekia pagerinti Europos maršrutų planus ir jų naudojimą. Neefektyvus oro erdvės planų ir oro maršrutinio tinklo naudojimas laikomas viena pagrindinių Europos skrydžių neefektyvumo priežasčių. Europos oro eismo valdymo (angl. ATM) sistema sudaryta iš daugelio atskirų oro navigacijos paslaugų teikėjų (angl. ANSP), o JAV sistema valdoma vieno oro navigacijos paslaugų teikėjo. Oro erdvės susiskirstymas pagal valstybių ribas daro skrydžio maršrutus neefektyvius dėl nepareikalautų oro maršrutų, skrydžio laiko, per didelio kuro sunaudojimo, CO ir NOx išsiskyrimo. Štai kodėl reikėtų pertvarkyti oro erdvę ir fiksuotų maršrutų tinklą, norint patenkinti oro erdvės operatorių poreikius ir išlaikyti reikalingą saugumo lygį. Šio straipsnio tikslas – parodyti skirtumus tarp suplanuotų skrydžių ir realių trajektorijų, įvertinant skrydžio atstumą, trukmę ir kuro sunaudojimą. Be to, buvo padaryta šių rodiklių apžvalga Europos ir JAV mastu.
Vilniaus Gedimino technikos universiteto Transporto inžinerijos mokslo krypties disertacijos gynimo taryba: Pirmininkas prof. habil. dr. Henrikas SIVILEVIČIUS (Vilniaus Gedimino technikos universitetas, transporto inžinerija -T 003). Nariai: prof. habil. dr. Algimantas FEDARAVIČIUS (Kauno technologijos universitetas, transporto inžinerija -T 003), doc. dr. Raimundas JUNEVIČIUS (Vilniaus Gedimino technikos universitetas, transporto inžinerija -T 003), habil. dr. Grzegorz Henryk KOPECKI (Žešuvo technologijos universitetas, Lenkija, transporto inžinerija -T 003), dr. Francisco Javier SAEZ NIETO (Kranfildo universitetas, Jungtinė Karalystė, transporto inžinerija -T 003). Disertacija bus ginama viešame Transporto inžinerijos mokslo krypties disertacijos gynimo tarybos posėdyje 2023 m. kovo 31 d. 13 val. Vilniaus Gedimino technikos universiteto senato posėdžių salėje.
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