2016
DOI: 10.2514/1.g001412
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Hybrid System Modeling and Estimation for Arrival Time Prediction in Terminal Airspace

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Cited by 11 publications
(10 citation statements)
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“…In both concepts, the accuracy of ETA significantly affects the system performance, and more accurate ETAs are expected. (Bai et al, 2016; Lee et al, 2016). The ATC systems usually rely on each aircraft's ETA information, but this paper demonstrates that the accuracy of ETA depends on the wind information each aircraft uses and aircraft type.…”
Section: Discussionmentioning
confidence: 99%
“…In both concepts, the accuracy of ETA significantly affects the system performance, and more accurate ETAs are expected. (Bai et al, 2016; Lee et al, 2016). The ATC systems usually rely on each aircraft's ETA information, but this paper demonstrates that the accuracy of ETA depends on the wind information each aircraft uses and aircraft type.…”
Section: Discussionmentioning
confidence: 99%
“…Since the motion of the aircraft is an SLHS with different flight modes, it is more reasonable to establish corresponding motion equations based on different flight modes. Therefore, many scholars use PMM to make predictions under SLHS [14,45,46]. Lymperopoulos et al [14] used the point mass model to model the aircraft under the stochastic hybrid system, combining the continuous state from the physical movement of the aircraft and the discrete state from the flight plan and the flight management system (FMS).…”
Section: Kinetic Modelmentioning
confidence: 99%
“…Lymperopoulos et al [14] used the point mass model to model the aircraft under the stochastic hybrid system, combining the continuous state from the physical movement of the aircraft and the discrete state from the flight plan and the flight management system (FMS). Lee et al [46] proposed an aircraft tracking and estimated time of arrival prediction algorithm based on a stochastic hybrid system model, deduced a nonlinear dynamics model of the continuous motion of the aircraft in each flight mode, and used the continuous state transition probability to model the discrete transition between flight modes.…”
Section: Kinetic Modelmentioning
confidence: 99%
“…Since the motion of the aircraft is an SLHS with different flight modes, it is more reasonable to establish motion equations corresponding to different flight modes. Therefore, many scholars use PMM to predict under SLHS [27][28][29]. Unified and comprehensive intent information is necessary for trajectory prediction.…”
Section: Kinetic Modelsmentioning
confidence: 99%