2018 IEEE/AIAA 37th Digital Avionics Systems Conference (DASC) 2018
DOI: 10.1109/dasc.2018.8569597
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Optimal assignment of 4D close-loop instructions to enable CDOs in dense TMAs

Abstract: Continuous descent operations (CDOs) with required times of arrival (RTAs) represent a potential solution to reduce the environmental impact in terminal maneuvering areas without degrading capacity. However, flight management systems require to know the remaining distance to the metering fix in order to compute the CDO complying with the CTA. This paper assesses the feasibility of replacing the current air traffic control sequencing and merging techniques, which are mainly based on open-loop vectoring, by a co… Show more

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Cited by 8 publications
(6 citation statements)
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“…where f : R nx×nu → R and f idle : R nx → R are the nominal and idle fuel flow, respectively; and CI is the cost index, which is a parameter chosen by the airspace user that reflects the relative importance of the cost of time with respect to fuel costs [1]. The CI is estimated by assuming that the aircraft was flying at the optimal speed in the cruise phase, as shown in [20].…”
Section: Fuel Burn Calculationmentioning
confidence: 99%
“…where f : R nx×nu → R and f idle : R nx → R are the nominal and idle fuel flow, respectively; and CI is the cost index, which is a parameter chosen by the airspace user that reflects the relative importance of the cost of time with respect to fuel costs [1]. The CI is estimated by assuming that the aircraft was flying at the optimal speed in the cruise phase, as shown in [20].…”
Section: Fuel Burn Calculationmentioning
confidence: 99%
“…where f : R nx×nu → R and f idle : R nx → R are the nominal and idle fuel flow, respectively; and CI is the cost index, which is a parameter chosen by the airspace user that reflects the relative importance of the cost of time with respect to fuel costs [2]. The CI is estimated by assuming that the aircraft was flying at the optimal speed in the cruise phase, as shown in [24].…”
Section: Additional Time In Tmamentioning
confidence: 99%
“…Given a known route (route length), and consequently a fixed distance to go, the optimization of the vertical profile (altitude and speed) can be formulated as an optimal control problem, which aims at computing the control time history of a system, here the aircraft, such that a cost function is minimized while satisfying some dynamic and operational constraints [25].…”
Section: Computation Of Cdo Speed Profilesmentioning
confidence: 99%