METHODOLOGY AND RESULTS OF PILOT MODEL IDENTIFICATION IN SEMIAUTOMATIC FLIGHT CONTROL

Authors

  • Valerii Azarskov National Aviation University
  • Grygorii Rudyuk ANTONOV Company

DOI:

https://doi.org/10.18372/2306-1472.64.8958

Keywords:

dynamic model, dynamic object, flight simulator, stabilization object, stochastic data, structural identification

Abstract

The article reviews statement of identification stage of pilot action models in the control loop, methodology, algorithms and certain results of its performance on flight simulator. New approach is offered for identification of operator dynamic models in moving object control loop. Distinctions are mainly related to multichannel expansion of traditional models that allows considering to a great extent the biological features of the operator.

Author Biographies

Valerii Azarskov, National Aviation University

Azarskov Valerii. Doctor of Engineering. Professor.
Aerospace Control Systems Department, National Aviation University, Kyiv, Ukraine.
Education: Kyiv Civil Aviation Engineers Institute, Kyiv, Ukraine (1968).
Research area: system identification, aircraft control systems, aviation and flight simulators and devices.

Grygorii Rudyuk, ANTONOV Company

Azarskov Valerii. Doctor of Engineering. Professor.
Aerospace Control Systems Department, National Aviation University, Kyiv, Ukraine.
Education: Kyiv Civil Aviation Engineers Institute, Kyiv, Ukraine (1968).
Research area: system identification, aircraft control systems, aviation and flight simulators and devices.

References

The modern theory of control systems / Ed. K.T. Leondesa. – M.: Mir, 1970. – 511 p. (In Russian).

Blokhin L.N. Optimal stabilization systems. – K.: "Technika", 1982. – 143 p. (In Russian).

Blokhin L.N. Synthesis of optimal robust systems in problems of ergonomics and stochastic stabilization // Cybernetics and Computer Science, 2000 – Vol. 122, – P. 28-50. (In Russian).

Azarskov V.N., Blokhin L.N., Zhiteckii L.S. Methodology of designing optimal stochastic stabilization systems. Monografіya. K.: NAU – 2006. – 432 p. (In Russian).

Azarskov V.N., Blokhin L.N., Burdin B.V. Pilot perception model of perturbed angular cabinmotion as a part of his information model. – M.: "Space Biology" – 1991. – Vol. 6. – P. 14-17. (In Russian).

Newton J.K., Gould L.A., Kayser. J. F. The theory of linear servo systems. – M.: FM, 1961. – 407 p. (In Russian).

Published

29-09-2015

How to Cite

Azarskov, V., & Rudyuk, G. (2015). METHODOLOGY AND RESULTS OF PILOT MODEL IDENTIFICATION IN SEMIAUTOMATIC FLIGHT CONTROL. Proceedings of National Aviation University, 64(3), 28–34. https://doi.org/10.18372/2306-1472.64.8958

Issue

Section

AEROSPACE SYSTEMS FOR MONITORING AND CONTROL