Robust Controller Design of Hypersonic Vehicle in Uncertainty Models

Nan Wu, Jia Yu

Abstract

This paper studies the controller of the air-breathing hypersonic vehicle. Taken the inertia into consideration, the control law of an air-breathing hypersonic vehicle is designed when the aircraft's appearance and aerodynamic parameters are changed. Due to the traditional controller is too dependent on the mathematic model of targets, the H2/H∞ control law of the air-breathing hypersonic vehicle is designed using the robust controller method. The rigid body model of the aircraft and the uncertainty model are researched in this paper. Then the corresponding robust controller is designed based on the uncertainty model in the case that the aircraft flies in different pitch angles. Finally, the stable flight characteristics of the hypersonic vehicle using the robust controller are verified in the complex flight conditions, compared to the general stability control system.

Download


Paper Citation


in Harvard Style

Wu N. and Yu J. (2018). Robust Controller Design of Hypersonic Vehicle in Uncertainty Models.In 3rd International Conference on Electromechanical Control Technology and Transportation - Volume 1: ICECTT, ISBN 978-989-758-312-4, pages 288-293. DOI: 10.5220/0006969302880293


in Bibtex Style

@conference{icectt18,
author={Nan Wu and Jia Yu},
title={Robust Controller Design of Hypersonic Vehicle in Uncertainty Models},
booktitle={3rd International Conference on Electromechanical Control Technology and Transportation - Volume 1: ICECTT,},
year={2018},
pages={288-293},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0006969302880293},
isbn={978-989-758-312-4},
}


in EndNote Style

TY - CONF

JO - 3rd International Conference on Electromechanical Control Technology and Transportation - Volume 1: ICECTT,
TI - Robust Controller Design of Hypersonic Vehicle in Uncertainty Models
SN - 978-989-758-312-4
AU - Wu N.
AU - Yu J.
PY - 2018
SP - 288
EP - 293
DO - 10.5220/0006969302880293