Abstract
Aircraft require significant quantities of fuel in order to generate the power required to sustain a flight. Burning this fuel causes the release of polluting particles to the atmosphere and constitutes a direct cost attributed to fuel consumption. The optimization of various aircraft operations in different flight phases such as cruise and descent, as well as terminal area movements, have been identified as a way to reduce fuel requirements, thus reducing pollution. The goal of this chapter is to briefly explain and apply different metaheuristic optimization algorithms to improve the cruise flight phase cost in terms of fuel burn. Another goal is to present an overview of the most popular commercial aircraft models. The algorithms implemented for different optimization strategies are genetic algorithms, the artificial bee colony, and the ant colony algorithm. The fuel burn aircraft model used here is in the form of a Performance Database. A methodology to create this model using a Level D aircraft research flight simulator is briefly explained. Weather plays an important role in flight optimization, and so this work explains a method for incorporating open source weather. The results obtained for the optimization algorithms show that every optimization algorithm was able to reduce the flight consumption, thereby reducing the pollution emissions and contributing to airlines’ profit margins.
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Abbreviations
- h (ft):
-
Altitude
- Pij:
-
Ants decision parameter
- Bg (ft, Mach or degrees):
-
Best global trajectory’s position
- P:
-
Bilinear interpolation weight
- va (kts or Kelvin):
-
Bilinear value to interpolate
- Dr (N):
-
Drag
- Rm (m):
-
Earth radio
- eij (hrs):
-
Flight Time difference
- F (kg):
-
Fuel burn
- Fij (kg):
-
Fuel burn for a given segment ij
- Cons (kg):
-
Fuel consumption
- ff (kg/hr):
-
Fuel flow
- g (m/s2):
-
Gravity
- GS (kts):
-
Ground Speed
- L (N):
-
Lift
- m (kg):
-
Mass
- c1:
-
Particle influence towards the global leader
- c2:
-
Particle influence towards the local leader
- D (Mach, degrees, ft):
-
Particle’s displacement
- X (Mach, degrees, ft):
-
Particle’s position
- C:
-
Pheromone
- R2:
-
Random parameter related to the global leader
- R1:
-
Random parameter related to the local leader
- Rω:
-
Random parameter related to the particle’s inertia
- v (kts):
-
South wind
- Bl (ft, Mach or degrees):
-
Best local trajectory’s position
- Th (N):
-
Thrust
- VTAS (kts):
-
True Air Speed
- w (kts):
-
Vertical wind
- u (kts):
-
West wind
- wd (kts):
-
Wind rates parallel to the aircraft
- χHDG (deg):
-
Aircraft azimuth
- α:
-
Algorithm convergence parameter
- β:
-
Algorithm convergence parameter
- ϕ (deg):
-
Latitude
- λ (deg):
-
Longitude
- ω:
-
Particle’s inertia
- γ:
-
Pheromone evaporation rate
- γTAS (deg):
-
Pitch
- μTAS (deg):
-
Roll
- η:
-
Thrust-specific fuel consumption
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Acknowledgements
We would like to thank the team of the Business-led Network of Centres of Excellence Green Aviation Research & Development Network (GARDN), and in particular Mr. Sylvan Cofsky for the funds received for this project (GARDN II—Project: CMC-21). This research was conducted at the Research Laboratory in Active Controls, Avionics and Aeroservoelasticity (LARCASE) in the framework of the global project “Optimized Descent and Cruise”. For more information please visit http://larcase.etsmtl.ca. We would like to thank Mr. Rex Haygate, Mr. Oussama Abdul-Baki, Mr. Reza Neshat and Mr. Yvan Blondeau from CMC-Electronics—Esterline. We would also like to thank Mr. Antoine Hamy, Mr. Audric Bunel, Mr. Charles Romain, Mr. Paul Mugnier, Mr. Jocelyn Gagné, Mr. Roberto Felix- Patron, Mr. Hugo Ruiz, Ms. Sonya Kessaci, and Mr. Oscar Carranza from LARCASE for their invaluable contributions. We also would like to thank the CONACYT (Mexico) and the FQRNT (Quebec, Canada) for their financial support.
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Murrieta-Mendoza, A., Botez, R.M. (2020). Commercial Aircraft Trajectory Optimization to Reduce Flight Costs and Pollution: Metaheuristic Algorithms. In: Vucinic, D., Rodrigues Leta, F., Janardhanan, S. (eds) Advances in Visualization and Optimization Techniques for Multidisciplinary Research. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-13-9806-3_2
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