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Published byJulie Murphy Modified over 9 years ago
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Mach Number Selection for Cruise Phase Using Ant Colony Algorithm with RTA Constrains Alejandro Murrieta-Mendoza, Antoine Hamy, Ruxandra M. Botez Université du Québec / ÉTS/ LARCASE 1
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Motivation Airline Expenses: 26% - 40% Fuel innovation.columbia.edu - Profit - Financial Planning - CO 2 - Global Share: 2% - NOx - H 2 0 - Hydrocarbons 2
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Motivation Canada: The Green Aviation Research & Development Network (GARDN) Develop technologies to reduce aircraft noise and emissions. Governmental Funding + Industrial Funding + University Expertise 3
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Introduction How to reduce fuel? www.turbosquid.com SA 3.0 Winglets Engines Improvements Morphing wings Trajectories and Airspace 4
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Introduction Conventional 3D Trajectories – Flight Plan. – Voice communication. 4D Time based Trajectories: IBO/TBO – Flight Plan – Advanced Systems – Required Time of Arrival 5
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Objectives Combination of Mach numbers that fulfill the RTA. ETA = RTA Reduce the fuel consumption – Reduce CO2, NOx, HC, etc… innovation.columbia.edu 6
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Trajectory Studied Cruise Phase – Bucharest – Grand Canary Constant Altitude 7
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Methodology Flight Cost Performance Database Experimental Flight Data 8
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Methodology Flight Cost 9
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Methodology How to manage the Mach Number? – Mach Number as a grid 10 Mach Number Options Lateral Flight Plan
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Methodology Ant Algorithm – Ants wander around for food sources. – Different ants find the food source. – Over time the shortest path is selected. – Use pheromone to keep track of the path The more ants are in a path, the more pheromone there is 11
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Methodology Ant Algorithm – Probability to select a given Mach Number – Pheromone Evaporation 12
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Results 2 Turbo-Fan Aircraft Real Flight Plan Waypoints were used – Weather obtained from flight plan RTA waypoint just before the ToD. Arbitrary imposed RTAs. 13
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Results 14 RTA: 4h20m0s – Tolerance: +/- 30 sec TailwindHeadwindHedwind Tailwind
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Results 15 RTA1: 4h20m (blue)RTA2: 4h24min (green) RTA3: 4h30m (red)RTA4: 4h36min (magneta)
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Results Flight Cost 16 FlightRTAFlight TimeDifference (s)Fuel Burn (T) 14h204h20m00s-16.057 24h254h24m59s116.848 34h304h30m40s4018.680 44h354h34m43s1719.431 Flight #Mach Number Flight Time Fuel Burn (Ton) 10.804h29m07s18.4 20.814h25m30s18.8 30.824h22m07s19.1 NO RTA RTA
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Conclusion In almost all cases, the ACO respected the RTAs imposed. The algorithm was able to improve fuel burn. – Less fuel burn equals less emissions. The algorithm takes local decisions. A global weather view is required to reduce the Mach Number variation. 17
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Thank You Q & A 18
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