STATIC OUTPUT FEEDBACK DESIGN OF ROBUST GAIN SCHEDULED CONTROL SYSTEM

Authors

  • О. I. Nadsadna Antonov Company

DOI:

https://doi.org/10.18372/1990-5548.47.10275

Keywords:

Gain scheduling, linear matrix inequalities, robustness, unmanned aerial vehicle

Abstract

Gain scheduling is one of the widely used controller design approaches with successfulapplication as well as in industrial and aerospace areas. It gives an opportunity to increase a degree ofthe system robustness without using adaptive loops. This paper considers gain-scheduling static outputfeedback controller design for linear parameter-varying system in terms of linear matrix inequalities. Theobtained controller guarantees an efficient unmanned aerial vehicle’s control under externaldisturbances within the flight envelope

Author Biography

О. I. Nadsadna, Antonov Company

Postgraduate student. Aircraft Control Systems Department, National Aviation University

References

O. P. Basanets, A. A. Tunik, M. M. Komnatska,“ LMI-based static output feedback design for rotating solid body,” presented at I-st Intern.Conf. Methods and Systems of Navigation and Motion Control, Kyiv, 2010, pp. 88–90.

R. W. Beard and T. W. Randal, Small Unmanned Aircraft : Theory and Practice. Princeton: Princeton University Press, 317 p.

S. Boyd, L. El. Ghaoui, E. Feron, and V. Balakrishnan, Linear matrix inequalities in system and control theory, Philadelphia: PA SIAM, 1994, 205 p.

X.Chen, J. Song and G. Cai, “Robust gain-scheduled autopilot design with LPV reference model for portable missile,” presented at IEEE Aerospace Conference, Montana, 2012. pр. 1–10.

J. Gadewadikar, F. Lewis, and M. Abu-Khalaf, “Necessary and sufficient conditions for H-infinity static output feedback control,” Journal of Guidance, Control and Dynamics, vol. 29, pp. 915–921, 2006.

J. Gadewadikar, and F. Lewis, “Aircraft flight controller tracking design using H-infinity static output-feedback,” ransactions of the Institute of Measurement and Control, vol. 28, no. 8, pp. 429–440, 2006.

M. M. Komnatska, “Flight control system design VIA LMI-approach,” Electronics and Control Systems, no. 3(37), pp. 49–52, 2013

M. O. Rauw, A Simulink Toolbox for Flight Dynamics and Control Analysis, oct 11, 2000, 263 p.

J. W. Rugh and S. J. Shamma, “Research on gain scheduling,” Automatica, vol. 36, pp. 1401–1425, 2000.

V. L. Syrmos, C. Abdallah, P. Dorato,“Static output feedback: a survey.” In Proc. of 33rd IEEE Conference on Decision and Control,Orlando, FL, 1997. pp. 837–842.

V. Saeed Vaseghi, Advanced Digital Signal Processing and Noise Reduction, Second Edition, John Wiley & Sons. 2000, pp. 297–330.

O. O. Abramovich, and A. A. Tunik, “Multi-Model Approach to Parametric Robust Optimization of Digital Flight Control Systems,” Journal of Automation and Information Sciences, Begell House Inc., no. 36(3), pp. 25–34, 2004.

Downloads

Issue

Section

AUTOMATIC CONTROL SYSTEMS