A Simulink model for an aircraft landing system using energy functions

V. I. George; Ciji Pearl Kurian; Joyson D'Souza; I. Thirunavukkarasu

doi:10.1109/ICIEA.2012.6360752

A Simulink model for an aircraft landing system using energy functions

V. I. George, Ciji Pearl Kurian, Joyson D'Souza, I. Thirunavukkarasu

Department of Instrumentation and Control Engineering, Manipal Institute of Technology, Manipal
Department of Electrical and Electronics Engineering, Manipal Institute of Technology, Manipal

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

2 Citations (Scopus)

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).

Original language	English
Title of host publication	Proceedings of the 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012
Pages	355-360
Number of pages	6
DOIs	https://doi.org/10.1109/ICIEA.2012.6360752
Publication status	Published - 2012
Event	2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012 - Singapore, Singapore Duration: 18-07-2012 → 20-07-2012

Conference

Conference	2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012
Country/Territory	Singapore
City	Singapore
Period	18-07-12 → 20-07-12

All Science Journal Classification (ASJC) codes

Electrical and Electronic Engineering

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10.1109/ICIEA.2012.6360752

Cite this

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title = "A Simulink model for an aircraft landing system using energy functions",

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).",

author = "George, {V. I.} and Kurian, {Ciji Pearl} and Joyson D'Souza and I. Thirunavukkarasu",

year = "2012",

doi = "10.1109/ICIEA.2012.6360752",

language = "English",

isbn = "9781457721175",

pages = "355--360",

booktitle = "Proceedings of the 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012",

note = "2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012 ; Conference date: 18-07-2012 Through 20-07-2012",

}

George, VI, Kurian, CP, D'Souza, J & Thirunavukkarasu, I 2012, A Simulink model for an aircraft landing system using energy functions. in Proceedings of the 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012., 6360752, pp. 355-360, 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012, Singapore, Singapore, 18-07-12. https://doi.org/10.1109/ICIEA.2012.6360752

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AU - D'Souza, Joyson

AU - Thirunavukkarasu, I.

PY - 2012

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N2 - 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).

AB - 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).

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BT - Proceedings of the 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012

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A Simulink model for an aircraft landing system using energy functions

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