Technical Papers
Sep 13, 2017

Nonlinear FOPID and Active Disturbance Rejection Hypersonic Vehicle Control Based on DEM Biogeography-Based Optimization

Publication: Journal of Aerospace Engineering
Volume 30, Issue 6

Abstract

This paper proposes an accurate system model independent resilient control approach with heuristic parameter optimization algorithm for air-breathing hypersonic vehicle tracking control. The control action is generated by the combination of nonlinear fractional-order proportional-integral-derivative (FOPID) and the active disturbance rejection control (ADRC). In particular, the FOPID controller increases two-degree-of-freedom variables, which improves the precision and stability of the control effect. The ADRC controller possesses aspects of the assimilation characteristics of the modern control theory and does not rely on the accurate mathematical model function, which is very suitable for a hypersonic vehicle system with parameter uncertainties and disturbances. Meanwhile, a new differential evolution exponential–cosine mixed migration (DEM) strategy for determining the biogeography-based optimization (BBO) migration rate to improve the optimization algorithm is proposed, which is mainly used for calculating tuning parameters of the FOPID ADRC. The improved hybrid algorithm is verified versus 14 benchmark functions and the practical optimization problems of the hypersonic vehicle vertical FOPID ADRC system are verified to illustrate the improved performance with the proposed approach. The effectiveness and robustness of the proposed method was verified by the simulation results.

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Acknowledgments

Special thanks to the support of the National Science Foundation project (Contract No. 51206007) and the China Scholarship Council (CSC) (Grant No. 20140625104), and to our colleagues for the suggestions and the research helps throughout the work.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 30Issue 6November 2017

History

Received: Feb 7, 2017
Accepted: May 12, 2017
Published online: Sep 13, 2017
Published in print: Nov 1, 2017
Discussion open until: Feb 13, 2018

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Authors

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Lecturer, School of Astronautics, Beihang Univ., Beijing 100191, China (corresponding author). E-mail: [email protected]
Master, School of Astronautics, Beihang Univ., Beijing 100191, China. E-mail: linjiaming1217@ buaa.edu.cn
Master, School of Astronautics, Beihang Univ., Beijing 100191, China. E-mail: [email protected]
Associate Professor, School of Aerospace, Dept. of Mechanical and Manufacturing Engineering, RMIT Univ., Bundoora East, Victoria 3083, Australia. E-mail: [email protected]
Xiaohong Guo [email protected]
Senior Engineer, State Key Laboratory of Astronautic Dynamic of China, 462 Xianning East Rd., Xincheng District, Xi’an 710043, China. E-mail: [email protected]

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