Continuous descent operations in high throughput environment

This report attempted to simulate the fuel-minimal descent and approach trajectory of a single B747-400 aircraft under ISA conditions. The aircraft is modelled as a point-mass model with parameters taken from the BADA database of EUROCONTROL. The Hermite-Simpson method is used to discretize the opti...

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Bibliographic Details
Main Author: Chan, Yong Cheng
Other Authors: School of Mechanical and Aerospace Engineering
Format: Final Year Project
Language:English
Published: 2014
Subjects:
Online Access:http://hdl.handle.net/10356/60252
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Institution: Nanyang Technological University
Language: English