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An investigation of a high-speed ground manoeuvre under optimal control

This paper studies the behaviour of a nonlinear aircraft model under optimal control for aircraft ground manoeuvres, specifically for high-speed runway exits. The aircraft’s behavior on the ground is captured by a fully parameterized 6-DOF nonlinear model. A pre-defined cost function is minimized us...

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Bibliographic Details
Main Authors: Zexin Huang, Matt Best, James Knowles
Format: Default Article
Published: 2019
Subjects:
Online Access:https://hdl.handle.net/2134/36401
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