Control of turbo shaft engine in hover flight using linear quadratic regulator (LQR)
المؤلفون المشاركون
Said, Muntasir Ali
al-Ata, al-Nadhir Khalaf Allah
Zayn, Abd al-Nasir Muhammad
المصدر
Libyan Journal of Engineering Science and Technology
العدد
المجلد 3، العدد 1 (30 يونيو/حزيران 2023)، ص ص. 7-12، 6ص.
الناشر
تاريخ النشر
2023-06-30
دولة النشر
ليبيا
عدد الصفحات
6
التخصصات الرئيسية
الملخص EN
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 state space formula to facilitate the analysis and design of a controller by LQR.
To explain the robustness of the controller, the impacts of disturbance are considered.
The calculations were performed using the MATLAB program.
The results show that using an LQR is a good solution for the SIMO gas turbine engine system, obtaining good stability, minimizing control effort, and refining the final behavior of the turboshaft engine.
نمط استشهاد جمعية علماء النفس الأمريكية (APA)
Said, Muntasir Ali& al-Ata, al-Nadhir Khalaf Allah& Zayn, Abd al-Nasir Muhammad. 2023. Control of turbo shaft engine in hover flight using linear quadratic regulator (LQR). Libyan Journal of Engineering Science and Technology،Vol. 3, no. 1, pp.7-12.
https://search.emarefa.net/detail/BIM-1501361
نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)
Said, Muntasir Ali…[et al.]. Control of turbo shaft engine in hover flight using linear quadratic regulator (LQR). Libyan Journal of Engineering Science and Technology Vol. 3, no. 1 (2023), pp.7-12.
https://search.emarefa.net/detail/BIM-1501361
نمط استشهاد الجمعية الطبية الأمريكية (AMA)
Said, Muntasir Ali& al-Ata, al-Nadhir Khalaf Allah& Zayn, Abd al-Nasir Muhammad. Control of turbo shaft engine in hover flight using linear quadratic regulator (LQR). Libyan Journal of Engineering Science and Technology. 2023. Vol. 3, no. 1, pp.7-12.
https://search.emarefa.net/detail/BIM-1501361
نوع البيانات
مقالات
لغة النص
الإنجليزية
الملاحظات
Includes bibliographical references : p. 12
رقم السجل
BIM-1501361
قاعدة معامل التأثير والاستشهادات المرجعية العربي "ارسيف Arcif"
أضخم قاعدة بيانات عربية للاستشهادات المرجعية للمجلات العلمية المحكمة الصادرة في العالم العربي
تقوم هذه الخدمة بالتحقق من التشابه أو الانتحال في الأبحاث والمقالات العلمية والأطروحات الجامعية والكتب والأبحاث باللغة العربية، وتحديد درجة التشابه أو أصالة الأعمال البحثية وحماية ملكيتها الفكرية. تعرف اكثر