NDLI: A Simulink model for an aircraft landing system using energy functions

Content Provider	IEEE Xplore Digital Library
Author	George, V.I. D'Souza, J. Kurian, C.P. Thirunavukkarasu, I.
Copyright Year	2012
Description	Author affiliation: Electrical and Electronics Engineering, MIT, Manipal University, India (D'Souza, J.) \|\| Instrumentation and Control Engineering, MIT, Manipal University, India (George, V.I.; Kurian, C.P.; Thirunavukkarasu, I.)
Abstract	A Simulink model for an aircraft landing system using Lyapunov function is discussed. This paper also illustrates the concepts of the Nonlinear Energy Based Control Method (NEM) and modifying the aircraft energy to automatically land an aircraft. The aircraft dynamics are expressed in the form of the Euler- Lagrange (EL) equations of motion, which are derived from the energy functions. The structure of a controller consists of an inner loop, energy loop and a tracking loop which controls the aircraft model dynamics. Using Matlab, Simulink and S functions, perform simulation for the control structure. The system considered in this paper is a Research Civil Aircraft Model (RCAM) developed by the Group for Aeronautical Research and Technology in Europe. (GARTEUR).
Starting Page	355
Ending Page	360
File Size	1175936
Page Count	6
File Format	PDF
ISBN	9781457721182
e-ISBN	9781457721199
DOI	10.1109/ICIEA.2012.6360752
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-07-18
Publisher Place	Singapore
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Aircraft Mathematical model Atmospheric modeling Aerospace control Aerospace electronics MATLAB Angle of attack Aircraft Landing Non-Liner Energy Based Control S-Function PID Control Pitch Velocity
Content Type	Text
Resource Type	Article

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