Structural-Parametric Synthesis Robust Flight Control System under Stochastic Disturbances and Inexact Measurements of the System’s State Vector

Authors

  • В. М. Азарсков Національний авіаційний університет
  • Т. А. Галагуз Національний авіаційний університет
  • А. А. Тунік Національний авіаційний університет

DOI:

https://doi.org/10.18372/2073-4751.1.11363

Abstract

The problem of synthesis of the optimal LQG controller for a system with stochastic disturbances («color noise»-type) and incomplete measurements of the state vector is solved. Then parametric robust optimization of obtained system is conducted to achieve stabilization and acceptable performance for nominal and parametrically disturbed plants using the same controller. Research is performed at the example of the small UAV (Unmanned Aerial Vehicle) flight control system

Author Biographies

В. М. Азарсков, Національний авіаційний університет

Інститут електроніки та систем управління, д-р техн. наук

А. А. Тунік, Національний авіаційний університет

Інститут електроніки та систем управління, д-р техн. наук

References

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How to Cite

Азарсков, В. М., Галагуз, Т. А., & Тунік, А. А. (2004). Structural-Parametric Synthesis Robust Flight Control System under Stochastic Disturbances and Inexact Measurements of the System’s State Vector. Problems of Informatization and Control, 1(10), 83–91. https://doi.org/10.18372/2073-4751.1.11363

Issue

Vol. 1 No. 10 (2004)

Section

Статті

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