Design of a flight management system to support four-dimensional trajectories
Visualitza/Obre
10.3846/16487788.2015.1015284
Inclou dades d'ús des de 2022
Cita com:
hdl:2117/86206
Tipus de documentArticle
Data publicació2015-03-01
Condicions d'accésAccés obert
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continguts d'aquesta obra estan subjectes a la llicència de Creative Commons
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Reconeixement-NoComercial-SenseObraDerivada 3.0 Espanya
Abstract
This paper presents the design and simulation of the functions of a flight Management System (FMS) in order to follow four-dimensional trajectories automatically. This is achieved by controlling the aircraft’s airspeed, altitude, heading and vertical speed in order to arrive to the merging point in a specified time. The system receives data from the aircraft and computes new control parameters based on mathematical equations and algorithms of prediction trajectories. Additional features have been added to the FMS-4D, such as the capability of predicting the arrival time taking into account previous flight parameters and speed/altitude constrains. Finally, a testing phase was carried out using a flight simulator in order to obtain the performance and results of the designed system.
CitacióAmaro, M., Rudinskas, D., Barrado, C. Design of a flight management system to support four-dimensional trajectories. "Aviation", 01 Març 2015, vol. 19, núm. 1, p. 58-65.
ISSN1648-7788
Versió de l'editorhttp://www.tandfonline.com
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