Title :
High-performance trajectory prediction for civil aircraft
Author :
Schuster, Wolfgang ; Ochieng, Washington ; Porretta, Marco
Author_Institution :
Imperial Coll. London, London, UK
Abstract :
High-performance trajectory prediction is at the core of strategic airspace capacity and safety enhancement. Current state-of-the-art trajectory prediction models are based on a three-dimensional point-mass model, using often predefined settings from existing databases rather than real-time information available onboard the aircraft to determine aircraft dynamics. As a result trajectory prediction performance is limited by the accuracy of these settings. This paper addresses this limitation and proposes a high-performance four-dimensional trajectory prediction model for civil aircraft. The model includes a new flight-control system and an enhanced flight-script. The latter incorporates new taxonomy and content enabling better definition of aircraft intent. The performance of the trajectory prediction model is assessed using data acquired during a real flight trial, and shown to be significantly better than the current models. It has the potential to meet the required navigation performance for departure, en-route and non-precision-approach phases of flight.
Keywords :
air traffic control; aircraft control; civil engineering; position control; civil aircraft intent; flight control system; high performance four dimensional trajectory prediction model; high performance trajectory prediction; nonprecision approach phases; real time information; safety enhancement; state-of-the-art trajectory prediction model; strategic airspace capacity; taxonomy; three dimensional point mass model; Aerospace control; Aircraft; Atmospheric modeling; Biological system modeling; Mathematical model; Predictive models; Trajectory;
Conference_Titel :
Digital Avionics Systems Conference (DASC), 2010 IEEE/AIAA 29th
Conference_Location :
Salt Lake City, UT
Print_ISBN :
978-1-4244-6616-0
DOI :
10.1109/DASC.2010.5655515