NDLI: Lateral Thrust and Aerodynamics Blended Control System Design Based on Variable Structure Model Following

Content Provider	IEEE Xplore Digital Library
Author	Yuhang Wang Yu Yao Kemao Ma
Copyright Year	2006
Description	Author affiliation: Control & Simulation Center, Harbin Inst. of Technol. (Yuhang Wang; Yu Yao; Kemao Ma)
Abstract	Variable structure model following technique is applied to the synthesis of a longitudinal autopilot for a missile with lateral thrust and aerodynamics blended. Firstly, the lateral thrust and aerodynamics blended control system model and the ideal reference model are established. Secondly, a variable structure model following controller is designed, and the stability and robustness of system are analyzed. Finally, the simulation model is developed. The simulation results show that variable structure model following control system using digital control is insensitive to the variations of the plant parameters, which can follow the reference model rapidly and has high robustness. The behavior of variable structure model following control system is highly affected by the selection of the control parameters
Starting Page	8183
Ending Page	8186
File Size	149575
Page Count	4
File Format	PDF
ISBN	1424403324
DOI	10.1109/WCICA.2006.1713569
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2006-06-21
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Subject Keyword	Aerodynamics Control system synthesis Missiles Robust control Robust stability Digital control Control systems Control theory Stability analysis Uncertainty blended control interception missile lateral thrust variable structure model following
Content Type	Text
Resource Type	Article

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