Design and control for rotor-fixed wing hybrid aircraft-Reference-Cited by-同舟云学术

Design and control for rotor-fixed wing hybrid aircraft

Published:2011-07 Issue:7 Volume:225 Page:831-847
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:

Wang Xinhua¹,Lin Hai¹

Affiliation:

1. Advanced Control Technology, Department of Electrical & Computer Engineering, National University of Singapore, Singapore

Abstract

This article presents a model of rotor-fixed wing hybrid aircraft, which can operate as a helicopter as well as transition to fixed-wing flight. The control mission includes: hover, vertical take-off and landing, forward flight, from hover to forward flight, and vice versa. A backstepping-based control method for the aircraft is designed to keep the flying height invariant during mode transitions from hover to forward flight and vice versa. The other control missions mentioned are not considered in this article.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/2041302510394742

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