2020 AIAA/IEEE 39th Digital Avionics Systems Conference (DASC) 2020
DOI: 10.1109/dasc50938.2020.9256711
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Prediction of the Propagation of Trajectory Uncertainty for Climbing Aircraft

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Cited by 7 publications
(5 citation statements)
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References 18 publications
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“…González-Arribas et al [10] proposed an algorithm for numerical optimal control, which simulates the optimal flight trajectory for different weight aircraft models under moving thunderstorm weather. Zeh et al [11] sampled 10000 climb tracks and used a neural network model to fit the trajectories of aircraft with different takeoff weights. The results showed that the fitting degree could reach 90% and the algorithm had high accuracy.…”
Section: State Of the Artmentioning
confidence: 99%
“…González-Arribas et al [10] proposed an algorithm for numerical optimal control, which simulates the optimal flight trajectory for different weight aircraft models under moving thunderstorm weather. Zeh et al [11] sampled 10000 climb tracks and used a neural network model to fit the trajectories of aircraft with different takeoff weights. The results showed that the fitting degree could reach 90% and the algorithm had high accuracy.…”
Section: State Of the Artmentioning
confidence: 99%
“…Among them, C f3 and C f4 is the fuel consumption coefficient in the descending section (unit: kg/min *N), as shown in Table 2 h represents the standard sea level pressure altitude (in feet) at the current position of the aircraft (Zeh et al, 2020). If N represents the number of engines installed on a certain type of aircraft, the total fuel consumption of the aircraft from time t 0 to time t 1 , according to BADA manual, the total fuel consumption of the approach segment can be expressed as Formula 16.…”
Section: Fuel Consumption Evaluation Modelmentioning
confidence: 99%
“…For decades, the impact of thrust, longitudinal speed and vertical speed is the subject of investigations with several optimization approaches [24][25][26]. Dancila and Botez [27], focus on minimizing steps during cruise and Bailey et al [28] developed algorithms to estimate aerodynamically optimized cruising altitudes, while the benefit of Continuous Climb Operation (CCO)s has been quantified by [29,30] Countless machine learning techniques were applied to historic flight tracks to identify fuel-efficient trajectories [31,32]. Fuel efficiency is optimized using dynamic programming [33] or pseudo spectral integration [34].…”
Section: State Of the Artmentioning
confidence: 99%