The optimal aircraft gas turbine engine control in low gas mode in the conditions of external additive noise-Reference-Cited by-同舟云学术

The optimal aircraft gas turbine engine control in low gas mode in the conditions of external additive noise

Published:2021-02-01 Issue:1 Volume:1745 Page:012039
ISSN:1742-6588
Container-title:Journal of Physics: Conference Series
language:
Short-container-title:J. Phys.: Conf. Ser.

Author:

Novikova S V,Tutubalin P I,Snegurenko A P,Yakhina R R

Abstract

Abstract The article is devoted to algorithm development to select an optimal control law of a gas turbine engine in the conditions of external additive noise and incomplete information regarding the values of control parameters. A step by-step algorithm for problem solving is given. The effectiveness of the algorithm is proved by numerical experiments.

Publisher

IOP Publishing

Subject

General Physics and Astronomy

Link

https://iopscience.iop.org/article/10.1088/1742-6596/1745/1/012039/pdf

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