Optimal TRACON Descent Procedures under Wind Uncertainty and Fuel Savings Factors
Published in Under review at AIAA Journal of Aircraft, 2026 · arXiv

Selects the flap-deployment trigger speeds and the glideslope-capture distance that minimize expected descent fuel under wind uncertainty, from six-degree-of-freedom aircraft and flight management system simulations.
* Corresponding author.
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@unpublished{pang2026fuel,
title = {Optimal TRACON Descent Procedures under Wind Uncertainty and Fuel Savings Factors},
author = {Pang, Y. and Clarke, J.},
note = {Under review at AIAA Journal of Aircraft},
year = {2026},
eprint = {2608.22480},
archivePrefix = {arXiv},
primaryClass = {eess.SY},
url = {https://arxiv.org/abs/2608.22480}
}