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Control of Turbo Shaft Engine in Hover Flight Using Linear Quadratic Regulator (LQR)
ISSN: 2789 - 2239
Publisher: author
Control of Turbo Shaft Engine in Hover Flight Using Linear Quadratic Regulator (LQR)
Indexed in
Technology and Engineering
ARTICLE-FACTOR
1.3
Article Basics Score: 2
Article Transparency Score: 2
Article Operation Score: 2
Article Articles Score: 3
Article Accessibility Score: 3
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International Category Code (ICC):
ICC-1802
Publisher: Bright Star University, Libya.
International Journal Address (IAA):
IAA.ZONE/2789404972239
eISSN
:
2789 - 2239
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Abstract
In this study, the Linear Quadratic Regulator (LQR) model has been obtained and the performance parameters have been estimated to minimize control effort. in general, controlling a gas turbine engine is difficult because its system is very coupled, nonlinear, and sensitive to the control inputs and external disturbances that might destabilize the system. due to these instabilities, it is crucial to use a control process that helps improve the system's performance, confirming stability and robustness. The main aim of this paper is to develop a control system design using Linear Quadratic Regulator (LQR) to stabilize the gas turbine engine near hover flight. To fulfill this objective, first of all, the nonlinear model of the turboshaft engine is linearized using the Taylor series theory. The engine model has been demonstrated by a series of first-order differential and algebraic equations, the model is linearized and extracted in the st...
