NDLI: Fliess Expansion-Based Bang-Bang Control Design and Its Application to Attitude Control of Missile

Content Provider	IEEE Xplore Digital Library
Author	Yu Yao Baoqing Yang Fenghua He Daizhan Cheng
Copyright Year	2006
Description	Author affiliation: Harbin Inst. of Technol. (Yu Yao; Baoqing Yang; Fenghua He)
Abstract	Motivated by the attitude control of missile, we consider the tracking problem of nonlinear systems via finite value control. First, the Fliess expansion is used to describe the outputs. Using piecewise finite value control and the quadratic criteria, the optimal control is obtained. Then for certain model uncertainty, the model predictive control is considered. On line predicted uncertain parameters are used to update the system's dynamics. The method developed is used to the control of missile. Simulation results show the effectiveness of the proposed method
Starting Page	188
Ending Page	192
File Size	147169
Page Count	5
File Format	PDF
ISBN	1424403324
DOI	10.1109/WCICA.2006.1712298
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	Bang-bang control Missiles Uncertainty Nonlinear control systems Predictive models Nonlinear systems Sampling methods Control systems Optimal control Predictive control Fliess functional expansion Nonlinear system model predictive tracking control
Content Type	Text
Resource Type	Article

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Fliess Expansion-Based Bang-Bang Control Design and Its Application to Attitude Control of Missile