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Smooth adaptive fixed time convergent controller design for BTT missiles with uncertainties

Published online by Cambridge University Press:  13 December 2019

Y. Yun Open the ORCID record for Y. Yun [Opens in a new window] ,
S. Tang Open the ORCID record for S. Tang [Opens in a new window] ,
J. Guo  and
Y. Yun
Y. Yun
Affiliation:
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
S. Tang*
Affiliation:
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
J. Guo
Affiliation:
School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China
Y. Yun
Affiliation:
State Grid Tianjin Power Maintenance Company, Tianjin 300232, China
*
tangsj@bit.edu.cn
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Abstract

A smooth adaptive sliding-mode-based controller is developed for BTT missiles considering nonlinear couplings and aerodynamic uncertainties, wherein fixed-time stability theory is synthesised into sliding-mode control algorithm, such that control variables follow the desired command within fixed-bounded convergence time. Unlike other terminal sliding-mode-related works, the bound of settling time is independent of initial states, indicating that performance metrics, for instance the convergence rate, can be evaluated in advance. The control input is designed to be intrinsically smooth, based on adaptive estimations, and therefore the problem of singularity and chattering is effectively eliminated. Simulation results demonstrate the satisfactory performance and validate the effectiveness of the designed approach.

Keywords

BTT controllerfixed time convergencerobust controlsmooth control input
Type
Research Article
Information
The Aeronautical Journal , Volume 124 , Issue 1273 , March 2020 , pp. 323 - 345
Copyright
© Royal Aeronautical Society 2019 

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References

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