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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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 |