Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics

المؤلفون المشاركون

Liu, Xiaodong
Wang, Yan
Huang, Wanwei
Jiao, Zongxia

المصدر

International Journal of Aerospace Engineering

العدد

المجلد 2015، العدد 2015 (31 ديسمبر/كانون الأول 2015)، ص ص. 1-7، 7ص.

الناشر

Hindawi Publishing Corporation

تاريخ النشر

2015-01-26

دولة النشر

مصر

عدد الصفحات

7

الملخص EN

This paper presents a novel robust attack angle control approach, which can effectively suppress the impacts from system uncertainties and servo-loop dynamics.

A second-order linear model of electromechanical servo loop is considered in the modeling and design processes.

With regard to the block-structure models facing attack angle control, the multiple robust surfaces and dynamic surface control (DSC) approaches are both employed.

By means of Lyapunov function method, the stability conditions of attack angle control systems are, respectively, given without/with considering the servo-loop dynamics in design process.

Computer simulation results present that, compared with the attack angle control scheme which does not consider the servo-loop dynamics in design process, the proposed scheme can guarantee that the whole attack angle control system possesses the better comprehensive performances.

Moreover, it is easy to be realized in engineering application.

نمط استشهاد جمعية علماء النفس الأمريكية (APA)

Liu, Xiaodong& Wang, Yan& Huang, Wanwei& Jiao, Zongxia. 2015. Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics. International Journal of Aerospace Engineering،Vol. 2015, no. 2015, pp.1-7.
https://search.emarefa.net/detail/BIM-1064503

نمط استشهاد الجمعية الأمريكية للغات الحديثة (MLA)

Liu, Xiaodong…[et al.]. Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics. International Journal of Aerospace Engineering No. 2015 (2015), pp.1-7.
https://search.emarefa.net/detail/BIM-1064503

نمط استشهاد الجمعية الطبية الأمريكية (AMA)

Liu, Xiaodong& Wang, Yan& Huang, Wanwei& Jiao, Zongxia. Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics. International Journal of Aerospace Engineering. 2015. Vol. 2015, no. 2015, pp.1-7.
https://search.emarefa.net/detail/BIM-1064503

نوع البيانات

مقالات

لغة النص

الإنجليزية

الملاحظات

Includes bibliographical references

رقم السجل

BIM-1064503