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Precise trajectory control for approach and landing is one of the difficult and key technologies in carrier-based aircraft design. Firstly, the dynamic inverse control method is briefly introduced. Secondly, the direct force control and unconventional maneuvering models are analyzed. Finally, the trajectory control simulation design is carried out according to three unconventional maneuvering flight states with different direct forces: longitudinal pitch direction, vertical translation and direct force mode. Finally, the simulation results show that the control method designed in this paper can control the automatic landing of aircraft well. The research work has certain engineering guiding value for the accurate trajectory landing control design of carrier-based aircraft.

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Research on the Control Mode Design of Direct Lift Glide Trajectory Based on Dynamic Inverse Control Method

  • 会议论文

  • 发表日期：

    2025年

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  • Li Hao,
  • Zhao LeTian,
  • Zhang Junhong,
  • Chen Hang,
  • Liu Shimin,
  • Zhang Wei

摘要

Precise trajectory control for approach and landing is one of the difficult and key technologies in carrier-based aircraft design. Firstly, the dynamic inverse control method is briefly introduced. Secondly, the direct force control and unconventional maneuvering models are analyzed. Finally, the trajectory control simulation design is carried out according to three unconventional maneuvering flight states with different direct forces: longitudinal pitch direction, vertical translation and direct force mode. Finally, the simulation results show that the control method designed in this paper can control the automatic landing of aircraft well. The research work has certain engineering guiding value for the accurate trajectory landing control design of carrier-based aircraft.