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Review Article | Publishing Language: Chinese

Research progress on guidance and control of fixed-wing manned and unmanned carrier-based aircraft landing

Zhibing ZHANG1Ziyang ZHEN2,3( )
Shenyang Aircraft Design and Research Institute, AVIC, Shenyang 110035, China
College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
National Key Laboratory of Aerospace Structures Mechanics and Control, Nanjing 210016, China
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Abstract

The technology of carrier-based aircraft landing is one of the core enablers for the development of modern aircraft carriers and amphibious fleets, directly impacting the safety, reliability, and operational efficiency of carrier-based aircraft. This paper systematically reviews the state-of-the-art technologies and key challenges in the landing of fixed-wing manned and unmanned carrier-based aircraft. First, it provides an overview of the current development status of fixed-wing manned/unmanned carrier-based landing systems and analyzes the differences in performance and mission requirements among various landing systems. Then, in terms of landing guidance technologies, the paper explores the application status of typical single-mode guidance methods and the development trends of multi-modal guidance technologies. In the area of landing control, it analyzes the architecture of typical flight control systems and the research progress of advanced flight control technologies. Furthermore, the study discusses the current research on technologies related to the safety of carrier landing systems. Finally, it summarizes the existing achievements and outlines future development directions, aiming to provide a reference for advancing fixed-wing carrier-based manned/unmanned landing technologies.

CLC number: V249;V241 Document code: A Article ID: 1000-6893(2025)13-532336-25

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Acta Aeronautica et Astronautica Sinica

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Cite this article:
ZHANG Z, ZHEN Z. Research progress on guidance and control of fixed-wing manned and unmanned carrier-based aircraft landing. Acta Aeronautica et Astronautica Sinica, 2025, 46(13). https://doi.org/10.7527/S1000-6893.2025.32336

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Received: 30 May 2025
Revised: 09 June 2025
Accepted: 13 June 2025
Published: 17 June 2025
© 2025 The Journal of Acta Aeronautica et Astronautica Sinica