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Landing control is a critical technical issue in the field of control. This paper investigates the design and performance characteristics of longitudinal artificial landing control systems under the FAPH and DP modes based on IDLC technology. Firstly, compared with Conventional Pitch Control (CPC), the flight control mechanism of DLC is studied, and a qualitative analysis of the improvement of the inherent model dynamic response by DLC is conducted. Secondly, the implementation method of DLC is provided, which involves the utilization of multi-control surface control allocation and optimization techniques. Finally, based on this approach, auxiliary landing control systems for FATH and DP modes are designed, and simulation studies of manual landing control are conducted using the MATLAB + FlightGear platform. The experiments demonstrate that the proposed method greatly enhances landing performance, reduces manual control workload, and possesses the capability to suppress ship wake.

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Design and Performance Analysis of IDLC-Based Landing Control System for Carrier-Based Aircraft

  • 会议论文

  • 发表日期：

    2025年

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  • Bing Wan,
  • Jie Wang,
  • Wei Han,
  • Yong Liang,
  • Xichao Su

摘要

Landing control is a critical technical issue in the field of control. This paper investigates the design and performance characteristics of longitudinal artificial landing control systems under the FAPH and DP modes based on IDLC technology. Firstly, compared with Conventional Pitch Control (CPC), the flight control mechanism of DLC is studied, and a qualitative analysis of the improvement of the inherent model dynamic response by DLC is conducted. Secondly, the implementation method of DLC is provided, which involves the utilization of multi-control surface control allocation and optimization techniques. Finally, based on this approach, auxiliary landing control systems for FATH and DP modes are designed, and simulation studies of manual landing control are conducted using the MATLAB + FlightGear platform. The experiments demonstrate that the proposed method greatly enhances landing performance, reduces manual control workload, and possesses the capability to suppress ship wake.