2018 IEEE/AIAA 37th Digital Avionics Systems Conference (DASC) 2018
DOI: 10.1109/dasc.2018.8569732
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Evaluation of the Applicability of a Modern Aircraft Performance Model to Trajectory Optimization

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Cited by 8 publications
(5 citation statements)
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“…There is no experiment in this paper to find the optimum number of elements of R. We selected two hundred distinct flight regimes consisting different values of altitude h, ISA temperature deviation ∆T, and aircraft mass m ac . Altitude and ISA deviation are sufficient to calculate pressure and temperature ratio through the following equations: (48) For each combination of δ, θ, and m ac , we calculate the corresponding Mach number limits. The minimum Mach number is in which the aircraft is cruising at the maximum lift coefficient available, C L,max .…”
Section: Methodsmentioning
confidence: 99%
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“…There is no experiment in this paper to find the optimum number of elements of R. We selected two hundred distinct flight regimes consisting different values of altitude h, ISA temperature deviation ∆T, and aircraft mass m ac . Altitude and ISA deviation are sufficient to calculate pressure and temperature ratio through the following equations: (48) For each combination of δ, θ, and m ac , we calculate the corresponding Mach number limits. The minimum Mach number is in which the aircraft is cruising at the maximum lift coefficient available, C L,max .…”
Section: Methodsmentioning
confidence: 99%
“…The analysis in this section are based on model-based approaches in BADA4 [45], which leverages OEM performance models of Airbus [46] and Boeing [47]. Developers of BADA4 showed the good approximation to these reference models [48]. The cruise phase of a flight is considered to be the equilibrium of both lateral and vertical forces:…”
Section: Cruise Fuel Consumption Dynamicsmentioning
confidence: 99%
“…To plan a feasible 4D trajectory in U-space, there is a need for uncrewed aircraft performance databases for all models of UAVs that are presented in U-space traffic [9]. In Europe, a similar issue has already been solved for commercial aviation for Air Traffic Control purposes via Base of Aircraft Data (BADA) and Trajectory Computation Infrastructure software [26,27]. U-space deals with a more complicated environment since UAVs do flights at VLL with a huge diversity of potential static and dynamic obstacles.…”
Section: Aircraft Performance and Maneuverabilitymentioning
confidence: 99%
“…• An aircraft performance model (APM) widely accepted by the ATM community, known as base of aircraft data (BADA) (Mouillet et al, 2018), was used for the experiments conducted in this PhD. Thus, the results obtained in this PhD may differ from those that could be obtained with a performance model provided by the manufacturer, which would reflect with a higher accuracy the actual behavior of the aircraft.…”
Section: I5 Scope and Limitations Of This Phd Thesismentioning
confidence: 99%
“…It covers 80% of aircraft types in the european civil aviation conference (ECAC) area, and it provides increased levels of precision in aircraft performance parameters over the entire flight envelope to enable modelling and simulation of advanced systems and future concepts. Mouillet et al (2018) assessed the viability of BADA v4 for trajectory optimization purposes. The results obtained with BADA v4 were compared with those obtained with original equipment manufacturer (OEM) reference performance data from certain Boeing aircraft types.…”
Section: Ii12 Aircraft Performance Modelmentioning
confidence: 99%