STUDY OF A CONTROLED COMPLEX MECHANICAL SYSTEM IN ANTI VIBRATORY DOMAIN - Application to a Hard Landing of an Aircraft

Cédric Lopez, François Malburet, André Barraco

2007

Abstract

This paper studies problematic of a mechanical system composed of different parts mechanically coupled and submitted to a high speed shock. After a shock, different parts of the system oscillate. If one of them is excited at a particular frequency, such as its proper frequency, important oscillations appear and can lead to the deterioration of the system by introducing important stresses. In this paper, we propose an analysis in order to understand this kind of problem and what we can do to avoid it. Firstly we discuss problematic and we expose the studied system. In a second time, we present model which allows us to understand the phenomenon by carrying out numerical simulations. Then we complete a comparative analysis of different methods of control. Prospects and problematic of real controlled device are studied. Finally experimental set up is described.

References

  1. Ghiringhelli, G.L. 2000. "Testing of semi active landing gear control for a general aviation aircraft". Journal of aircraft vol. 37, No 4. (July-August).
  2. Giua, A.; M. Melas and C. Seatzu. 2004. "Design of a control law for a semi active suspension system using a solenoid valve damper". Proceeding 2004 IEEE Conference on Control Applications, Taipei, Taiwan. (Sept.).
  3. Guglielmino, E. and K.A. Edge. 2004. "A controlled friction damper for vehicle applications". Control Engineering Practice 12, pp 431-443.
  4. Kim, W.S.; W.S. Lee and J.H. Kim. 2003. "Control of an Active Vehicle Suspension Using Electromagnetic Motor". ICCAS2003, Gyeongju, Korea. (Oct. 22-25).
  5. Kruger, W. 2000. "Integrated Design Process for the Development of Semi-Active Landing Gears for Transport Aircraft". Thesis Institut für Flugmechanik und Flugregelung der Universität Stuttgart. 122p.
  6. Yagiz, N. 2004. "Comparison and Evaluation of Different Control Strategies on a Full Vehicle Model with Passenger Seat using Sliding Modes". International Journal of Vehicle Design, vol. 34, No 2, pp 168-182.
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Paper Citation


in Harvard Style

Lopez C., Malburet F. and Barraco A. (2007). STUDY OF A CONTROLED COMPLEX MECHANICAL SYSTEM IN ANTI VIBRATORY DOMAIN - Application to a Hard Landing of an Aircraft . In Proceedings of the Fourth International Conference on Informatics in Control, Automation and Robotics - Volume 3: ICINCO, ISBN 978-972-8865-84-9, pages 33-39. DOI: 10.5220/0001619600330039


in Bibtex Style

@conference{icinco07,
author={Cédric Lopez and François Malburet and André Barraco},
title={STUDY OF A CONTROLED COMPLEX MECHANICAL SYSTEM IN ANTI VIBRATORY DOMAIN - Application to a Hard Landing of an Aircraft},
booktitle={Proceedings of the Fourth International Conference on Informatics in Control, Automation and Robotics - Volume 3: ICINCO,},
year={2007},
pages={33-39},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0001619600330039},
isbn={978-972-8865-84-9},
}


in EndNote Style

TY - CONF
JO - Proceedings of the Fourth International Conference on Informatics in Control, Automation and Robotics - Volume 3: ICINCO,
TI - STUDY OF A CONTROLED COMPLEX MECHANICAL SYSTEM IN ANTI VIBRATORY DOMAIN - Application to a Hard Landing of an Aircraft
SN - 978-972-8865-84-9
AU - Lopez C.
AU - Malburet F.
AU - Barraco A.
PY - 2007
SP - 33
EP - 39
DO - 10.5220/0001619600330039