Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics

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-str...

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Main Authors: Xiaodong Liu, Yan Wang, Wanwei Huang, Zongxia Jiao
Format: Article
Language:English
Published: Wiley 2015-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2015/284863
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author Xiaodong Liu
Yan Wang
Wanwei Huang
Zongxia Jiao
author_facet Xiaodong Liu
Yan Wang
Wanwei Huang
Zongxia Jiao
author_sort Xiaodong Liu
collection DOAJ
description 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.
format Article
id doaj-art-941b6d7db6fd480a85d1909abed00ab1
institution Kabale University
issn 1687-5966
1687-5974
language English
publishDate 2015-01-01
publisher Wiley
record_format Article
series International Journal of Aerospace Engineering
spelling doaj-art-941b6d7db6fd480a85d1909abed00ab12025-02-03T01:01:28ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742015-01-01201510.1155/2015/284863284863Research on Aircraft Attack Angle Control Considering Servo-Loop DynamicsXiaodong Liu0Yan Wang1Wanwei Huang2Zongxia Jiao3Beijing Aerospace Automatic Control Institute, Beijing 100854, ChinaSchool of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaBeijing Aerospace Automatic Control Institute, Beijing 100854, ChinaSchool of Automation Science and Electrical Engineering, Beihang University, Beijing 100191, ChinaThis 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.http://dx.doi.org/10.1155/2015/284863
spellingShingle Xiaodong Liu
Yan Wang
Wanwei Huang
Zongxia Jiao
Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics
International Journal of Aerospace Engineering
title Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics
title_full Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics
title_fullStr Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics
title_full_unstemmed Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics
title_short Research on Aircraft Attack Angle Control Considering Servo-Loop Dynamics
title_sort research on aircraft attack angle control considering servo loop dynamics
url http://dx.doi.org/10.1155/2015/284863
work_keys_str_mv AT xiaodongliu researchonaircraftattackanglecontrolconsideringservoloopdynamics
AT yanwang researchonaircraftattackanglecontrolconsideringservoloopdynamics
AT wanweihuang researchonaircraftattackanglecontrolconsideringservoloopdynamics
AT zongxiajiao researchonaircraftattackanglecontrolconsideringservoloopdynamics