NDLI: Application of the feedback decoupling method in the attitude control of the rolling aircraft

Content Provider	IEEE Xplore Digital Library
Author	Jie Guo Shengjing Tang
Copyright Year	2012
Description	Author affiliation: Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education, School of Aerospace Engineering, Beijing Institute of Technology, China (Jie Guo; Shengjing Tang)
Abstract	Considering the existence of the coupling effects that are distributed in the seeker loop, the actuators, the aerodynamic forces and the sensitive devices of the rolling aircraft, it will to some extend affect the control quality and add difficulty to the design of the control system. And in condition of strong coupling, the success or failure of the whole control system may even be affected. This paper focuses on the feedback decoupling theory the in time domain and its application in attitude control of the rolling aircraft. Firstly, the linear state feedback decoupling theory is discussed based on square system. Subsequently, for a special integral system, a simple and intuitive method is proposed to realize pole assignment of the decoupling system and obtain the expected closed loop characteristics through the comparison of closed-loop characteristic polynomial. Then, the dynamics model of the rolling aircraft is established including the body dynamics link and the actuator dynamics link. At last, an integrated design example is given as an application in the rolling aircraft control system. The simulation results have verified the validity of this method.
Starting Page	371
Ending Page	375
File Size	273965
Page Count	5
File Format	PDF
ISBN	9781467301985
e-ISBN	9781467301992
DOI	10.1109/ICSAI.2012.6223637
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2012-05-19
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Couplings Rolling aircraft State feedback State feedback decoupling Transfer functions Decoupling control Dynamic coupling model Feedback control Mathematical model Aircraft Aerospace control
Content Type	Text
Resource Type	Article

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