A Simulink model for an aircraft landing system using energy functions

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

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (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 languageEnglish
Title of host publicationProceedings of the 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012
Pages355-360
Number of pages6
DOIs
Publication statusPublished - 2012
Event2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012 - Singapore, Singapore
Duration: 18-07-201220-07-2012

Conference

Conference2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012
CountrySingapore
CitySingapore
Period18-07-1220-07-12

Fingerprint

Aircraft landing systems
Aircraft models
Aircraft
Lyapunov functions
Equations of motion
Controllers

All Science Journal Classification (ASJC) codes

  • Electrical and Electronic Engineering

Cite this

George, V. I., Kurian, C. P., 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 (pp. 355-360). [6360752] https://doi.org/10.1109/ICIEA.2012.6360752
George, V. I. ; Kurian, Ciji Pearl ; D'Souza, Joyson ; Thirunavukkarasu, I. / A Simulink model for an aircraft landing system using energy functions. Proceedings of the 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012. 2012. pp. 355-360
@inproceedings{4c675176736b4f539feb6e3ab161e1c1,
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",

}

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

A Simulink model for an aircraft landing system using energy functions. / George, V. I.; Kurian, Ciji Pearl; D'Souza, Joyson; Thirunavukkarasu, I.

Proceedings of the 2012 7th IEEE Conference on Industrial Electronics and Applications, ICIEA 2012. 2012. p. 355-360 6360752.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

TY - GEN

T1 - A Simulink model for an aircraft landing system using energy functions

AU - George, V. I.

AU - Kurian, Ciji Pearl

AU - D'Souza, Joyson

AU - Thirunavukkarasu, I.

PY - 2012

Y1 - 2012

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).

UR - http://www.scopus.com/inward/record.url?scp=84871680779&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84871680779&partnerID=8YFLogxK

U2 - 10.1109/ICIEA.2012.6360752

DO - 10.1109/ICIEA.2012.6360752

M3 - Conference contribution

AN - SCOPUS:84871680779

SN - 9781457721175

SP - 355

EP - 360

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

ER -

George VI, Kurian CP, D'Souza J, Thirunavukkarasu I. 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. 2012. p. 355-360. 6360752 https://doi.org/10.1109/ICIEA.2012.6360752