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Stable and accurate tracking control of tail-sitter aircraft in all flight modes

Xu Zou (The School of Civil Aviation, Northwestern Polytechnical University, Xi'an, China)
Zhenbao Liu (The School of Civil Aviation, Northwestern Polytechnical University, Xi'an, China and Research and Development Institute, Northwestern Polytechnical University, Shenzhen, China)
Qingqing Dang (The School of Civil Aviation, Northwestern Polytechnical University, Xi'an, China)
Lina Wang (The School of Civil Aviation, Northwestern Polytechnical University, Xi'an, China)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 19 January 2023

Issue publication date: 2 May 2023

125

Abstract

Purpose

This paper aims to design a global controller that is operational throughout all flight modes and less dependent on an accurate model.

Design/methodology/approach

By adopting the interconnection and damping assignment passivity-based control (IDA-PBC) technology and compensating extra inputs for handling the unknown dynamics and time-varying disturbances, a model-free control (MFC)-based global controller is proposed.

Findings

Test results indicate that the designed controllers are more suitable for actual flight as they have smaller position tracking errors and energy consumption in all flight phases than the excellent model-free controller intelligent-PID.

Practical implications

The designed global controller, which works in all flight modes without adjusting its structure and parameters, can realize a stable and accurate tracking control of a tail-sitter and improve the resistance to unknown disturbances and model uncertainties.

Originality/value

The newly-designed controller is considered as an enhanced version of the traditional MFC. It further improves the control effect by using the poorly known dynamics of the system and choosing the IDA-PBC as the control auxiliary input. This method eliminates the unnecessary dynamics to continuously stabilize the vehicle with suitable energy consumption covering its entire flight envelope.

Keywords

Acknowledgements

This work is supported by the National Nature Science Foundation of China (Grant no.52072309), the Supported by Shenzhen Fundamental Research Program (No. JCYJ20190806152203506), the Supported by Aeronautical Science Foundation of China (No. ASFC-2018ZC53026) and the Supported by the Natural Science Basis Research Plan in Shaanxi Province of China (2021JQ-086).

Citation

Zou, X., Liu, Z., Dang, Q. and Wang, L. (2023), "Stable and accurate tracking control of tail-sitter aircraft in all flight modes", Aircraft Engineering and Aerospace Technology, Vol. 95 No. 6, pp. 858-868. https://doi.org/10.1108/AEAT-08-2022-0227

Publisher

:

Emerald Publishing Limited

Copyright © 2023, Emerald Publishing Limited

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