Nonsingular terminal sliding mode control for reusable launch vehicle with atmospheric disturbances-Reference-Cited by-同舟云学术

Nonsingular terminal sliding mode control for reusable launch vehicle with atmospheric disturbances

Published:2017-05-08 Issue:11 Volume:232 Page:2019-2033
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

You Ming¹,Zong Qun¹,Tian Bailing¹,Zeng Fanlin²

Affiliation:

1. School of Electrical and Information Engineering, Tianjin University, Tianjin, China

2. Tianjin Key Laboratory of Information Sensing and Intelligent Control, School of Automation and Electrical Engineering, Tianjin University of Technology and Education, Tianjin, China

Abstract

The controller design for reusable launch vehicles is challenging due to enormous amounts of model parameter uncertainties and atmospheric disturbances. This paper first derives six-degree-of-freedom model of a reusable launch vehicle with atmospheric disturbances. Next, four kinds of atmospheric disturbances are introduced and wind models are established respectively. For attitude control of the reusable launch vehicle, a nonsingular terminal sliding mode controller is designed with stability guaranteed. Finally, simulation results show a satisfactory performance for the attitude tracking of the reusable launch vehicle with atmospheric disturbances.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/0954410017708211

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