Aircraft trajectory optimization during descent using a Kriging-model-based-genetic algorithm

A time-series flight trajectory technique was developed for use in a civil aircraft during descent. The three-degree-of-freedom (3-DoF) equations of motion were solved via time-series prediction of aerodynamic forces. In the present evaluation, the microburst effect during the descent was considered...

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Bibliographic Details
Main Authors: Othman, Norazila, Mansor, Shuhaimi, Ab. Wahid, Mastura, Abdul Latif, Ainullotfi, Wan Omar, Wan Zaidi, Mohd. Jaafar, Mohammad Nazri, Wan Ali, Wan Khairuddin, Dahalan, Md. Nizam, Mohd. Nasir, Mohd. Nazri, Kanazaki, Masahiro
Format: Article
Published: Jurnal Mekanikal 2018
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Online Access:http://eprints.utm.my/id/eprint/82296/
https://jurnalmekanikal.utm.my
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