A linear quadratic regulator (LQR) based adaptive optimal control method for aircraft engine is presented. Firstly, an LQR controller is designed for the nominal system, based on which, a adaptive controller is designed by using the back-stepping technique. With the proposed method, the system uncertainties and external disturbances can be compensated, and the actual controller can converge to the LQR controller as close as possible. Finally, a turbofan engine simulation is considered to illustrate the effectiveness of the proposed method.
LQR-Based Adaptive Optimal Control for Aircraft Engine
Lect. Notes Electrical Eng.
Chinese Intelligent Systems Conference ; 2023 ; Ningbo, China October 14, 2023 - October 15, 2023
08.10.2023
9 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
ADAPTIVE AIRCRAFT ENGINE AND AIRCRAFT HAVING AN ADAPTIVE ENGINE
Europäisches Patentamt | 2016
|Adaptive aircraft engine and aircraft having an adaptive engine
Europäisches Patentamt | 2019
|