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

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...

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Veröffentlicht in:	Journal of physics. Conference series 2021-02, Vol.1745 (1), p.12039
Hauptverfasser:	Novikova, S V, Tutubalin, P I, Snegurenko, A P, Yakhina, R R
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft control Algorithms Control theory Engine control Gas turbine engines Optimal control Physics
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Beschreibung
Zusammenfassung:	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.
ISSN:	1742-6588 1742-6596
DOI:	10.1088/1742-6596/1745/1/012039