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...
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 |
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Format: | Article |
Published: |
Jurnal Mekanikal
2018
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Subjects: |
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