PARAMETRICAL SYNTHESIS OF ROBUST SYSTEM FOR STABILIZATION OF AIRCRAFT EQUIPMENT

Authors

  • O. A. Sushchenko National Aviation University, Kyiv
  • S. D. Yehorov National Aviation University, Kyiv

DOI:

https://doi.org/10.18372/1990-5548.57.13239

Keywords:

Stabilization system, parametrical optimization, robust control, aiircraft equipment, stabilization errors

Abstract

The paper deals with parametrical synthesis of robust system assigned for stabilization of aircraft equipment. The mathematical model of the stabilization plant is represented. The algorithm of parametrical synthesis of robust system is given. Features of the optimization procedure including choice of programming tools are reprsented. The optimization criterion of parametrical synthesis of robust system is shown. Criteria of performance of the synthesied system including stabilization errors are analysed. Features of simulation tests are discussed. Results of synthesied system simulation are represented.  The obtained results can be useful for moving vehicles of the wide class.

Author Biographies

O. A. Sushchenko, National Aviation University, Kyiv

Aerospace Control Systems Department, Education&Research Institute of Air Navigation, Electronics and Telecommunications

Doctor of Engineering. Professor

S. D. Yehorov, National Aviation University, Kyiv

Avionics Department, Education&Research Institute of Air Navigation, Electronics and Telecommunications

Senior Teacher

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Issue

Vol. 3 No. 57 (2018)

Section

AUTOMATIC CONTROL SYSTEMS

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