Optimal observer-based control design for aircraftlateral motion

Authors

  • M. M. Komnatska National Aviation University
  • I. V. Kiliian National Aviation University
  • Y. A. Berezanskyi National Aviation University

DOI:

https://doi.org/10.18372/2073-4751.3.10315

Abstract

The paper presents an alternative approach of observer-based flight control system design. Thisapproach is based on the application of linear matrix inequality technique. The design proceduretreats the design of both observer and controller by solving the set of linear inequalitiessimultaneously. The proposed approach is free of observer poles placement location. Simulationresults demonstrate the validity and effectiveness of the proposed design approach

Author Biography

M. M. Komnatska, National Aviation University

Ph. D.

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How to Cite

Komnatska, M. M., Kiliian, I. V., & Berezanskyi, Y. A. (2015). Optimal observer-based control design for aircraftlateral motion. Problems of Informatization and Control, 3(51), 67–73. https://doi.org/10.18372/2073-4751.3.10315

Issue

Vol. 3 No. 51 (2015)

Section

Статті

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