Aircraft simulation and control

This dissertation aims at F-16 fighter to design controller and to make simulation for analyzing its performance under specific condition. Nonlinear plants model of F-16 derived from the kinematics and dynamics of aircraft is first given, which provides a necessary precondition for analyzing and res...

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Bibliographic Details
Main Author: Zhao, Liang.
Other Authors: Wang Jianliang
Format: Theses and Dissertations
Language:English
Published: 2009
Subjects:
Online Access:http://hdl.handle.net/10356/18758
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Institution: Nanyang Technological University
Language: English