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Thesis-1985-Elsayed.pdf (5.89 MB)

Aircraft trajectory optimization

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thesis
posted on 2018-05-09, 09:53 authored by M.A.N. Elsayed
A typical aircraft flight consists of three phases, namely climb, cruise and descent. The purpose of this research was to study the control schedules for a transport aircraft which would result in least fuel expenditure in each flight-segment. [Continues.]

Funding

Science and Engineering Research Council.

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Publisher

© M.A.N. Elsayed

Publisher statement

This work is made available according to the conditions of the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International (CC BY-NC-ND 4.0) licence. Full details of this licence are available at: https://creativecommons.org/licenses/by-nc-nd/4.0/

Publication date

1985

Notes

A Doctoral Thesis. Submitted in partial fulfilment of the requirements for the award of Doctor of Philosophy at Loughborough University.

Language

  • en

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    Aeronautical and Automotive Engineering Theses

    Categories

    Keywords

    untaggedEngineering not elsewhere classified

    Licence

    CC BY-NC-ND 4.0

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