Automatic aircraft landing control using nonlinear energy method

This paper presents the integration of longitudinal and lateral dynamics controller designed using Nonlinear Energy Method (NEM) for a research civil aircraft. This controller ensures the core attitudes of the aircraft such as roll, pitch, yaw and airspeed follows their reference value determined b...

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Bibliographic Details
Main Authors: Jones, Lim Jen Nee, Akmeliawati, Rini, Tan, Chee Pin
Format: Conference or Workshop Item
Language:English
English
Published: IEEE 2010
Subjects:
Online Access:http://irep.iium.edu.my/5379/1/MSC2010_JN.pdf
http://irep.iium.edu.my/5379/4/16296-Automatic_aircraft_landing_control_using_nonlinear_energy_method__SCOPUS.pdf
http://irep.iium.edu.my/5379/
http://ieeexplore.ieee.org/xpls/abs_all.jsp?arnumber=5611294&tag=1
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