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- W2322897785 abstract "This paper studies and compares optimal climb and descent trajectories that conform to the Air Traffic Control (ATC) procedures and minimize fuel consumption, emissions, flight time, and/or flight distance. Tradeoffs among these different performance criteria are examined. In addition, closed-loop sensitivities are used to evaluate the likely variations of fuel burns, emissions, and flight times when optimized trajectories are tracked in actual flights. In this paper, a point-mass model of conventional commercial aircraft is used, together with available models of aircraft performance and emissions. Aircraft vertical profiles in the ATC system are described through a series of flight segments. The segment parameters are optimized to minimize fuel burn, emissions, flight time, flight distance, and/or their linear combinations, subject to aircraft equations of motion, aircraft performance limitations, and appropriate boundary conditions. A gradient method is devised for numerical solutions. In calculating the closed-loop sensitivities, the method of feedback linearization is used to model aircraft guidance strategies." @default.
- W2322897785 created "2016-06-24" @default.
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- W2322897785 date "2011-06-04" @default.
- W2322897785 modified "2023-09-27" @default.
- W2322897785 title "Optimization and Sensitivity Analysis of Climb and Descent Trajectories for Reducing Fuel Burn and Emissions" @default.
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- W2322897785 doi "https://doi.org/10.2514/6.2011-6879" @default.
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