Aircraft trajectory simulator using a three degrees of freedom aircraft point mass model
Javier García‐Heras, Francisco Javier Sáez Nieto, Ricardo Román Cordón
Abstract
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Javier García‐Heras, Francisco Javier Sáez Nieto, Ricardo Román Cordón
Abstract
Open-access reader
Aircraft Operators Companies (AOCs) are always willing to keep the cost of a flight as low as possible. These costs could be modelled using a function of the fuel consumption, time of flight and fixed cost (over flight cost, maintenance, etc.). These are strongly dependant on the atmospheric conditions, the presence of winds and the aircraft performance. For this reason, much research effort is being put in the development of numerical and graphical techniques for defining the optimal trajectory.
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Aircraft Operators Companies (AOCs) are always willing to keep the cost of a flight as low as possible. These costs could be modelled using a function of the fuel consumption, time of flight and fixed cost (over flight cost, maintenance, etc.). These are strongly dependant on the atmospheric conditions, the presence of winds and the aircraft performance. For this reason, much research effort is being put in the development of numerical and graphical techniques for defining the optimal trajectory.
Key concepts: Trajectory, Fuel efficiency, Flight simulator, Point (geometry), Trajectory optimization, Computer science, Function (biology), Atmospheric model