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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書目詳細資料
主要作者: Chan, Yong Cheng
其他作者: School of Mechanical and Aerospace Engineering
格式: Final Year Project
語言:English
出版: 2014
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在線閱讀:http://hdl.handle.net/10356/60252
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機構: Nanyang Technological University
語言: English