AIAA Guidance, Navigation, and Control Conference 2011
DOI: 10.2514/6.2011-6660
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High-Speed Prediction of Air Traffic for Real-Time Decision Support

Abstract: The ability to rapidly generate traffic predictions is expected to be central for implementing next-generation air traffic management functionality, both on the ground and aboard aircraft. While high-end computers can be used for this purpose, emerging capabilities of computational hardware such as Graphics Processing Units, together with Cloud Computing concepts can be exploited to realize substantial acceleration of trajectory computations at a modest cost increment. This paper discusses the development of a… Show more

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Cited by 8 publications
(5 citation statements)
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“…For example, an alternate method tested in the development of this work involved using an established departure uncertainty distribution 20 to perturb the departure time of all flights. This perturbation was repetitively simulated using the Computational Appliance for Rapid Prediction of Aircraft Trajectories (CARPAT) 21 to develop sector demand statistics. This method includes additional, historically-based uncertainties such as aircraft speed uncertainty.…”
Section: Iiic Alternate Methods Of Uncertainty Data Generationmentioning
confidence: 99%
“…For example, an alternate method tested in the development of this work involved using an established departure uncertainty distribution 20 to perturb the departure time of all flights. This perturbation was repetitively simulated using the Computational Appliance for Rapid Prediction of Aircraft Trajectories (CARPAT) 21 to develop sector demand statistics. This method includes additional, historically-based uncertainties such as aircraft speed uncertainty.…”
Section: Iiic Alternate Methods Of Uncertainty Data Generationmentioning
confidence: 99%
“…We use kinematic models of aircraft navigation with simplified dynamics and control, similar to the models developed by others. 13,14,15 The aircraft state vector is defined as…”
Section: B Modelingmentioning
confidence: 99%
“…We use kinematic models of aircraft navigation with simplified dynamics and control, similar to the models developed by others (Bilmoria, Banavar, Chatterji, Sheth, & Grabbe, 2000;Chatterji, Sridhar, & Bilimoria, 1996;Tandale, Wiraatmadja, Menon, & Rios, 2011). In the following description, we present differential equations in continuous time t; for implementation purposes, they are converted to difference equations using a sampling time of 10 s. The aircraft state vector is defined as…”
Section: Aircraft Modelingmentioning
confidence: 99%