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Prediction and Compensation Model of Longitudinal and Lateral Deck Motion for Automatic Landing Guidance System

Author

Listed:
  • Chen Cheng

    (School of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China)

  • Zian Wang

    (China Academy of Launch Vehicle Technology, Beijing 100076, China)

  • Zheng Gong

    (Department of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

  • Pengcheng Cai

    (Department of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China)

  • Chengxi Zhang

    (School of Electronics and Information Engineering, Harbin Institute of Technology, Shenzhen 518055, China)

Abstract

This paper mainly studies the longitudinal and lateral deck motion compensation technology. In order to ensure the safe landing of the carrier-based aircrafts on the flight decks of carriers during the landing process, it is necessary to introduce deck motion information into the guidance law information of the automatic landing guidance system when the aircraft is about to land so that the aircraft can track the deck motion. To compensate the influence of the height change in the ideal landing point on the landing process, the compensation effects of the deck motion compensators with different design parameters are verified by simulation. For further phase-lead compensation for the longitudinal automatic landing guidance system, a deck motion predictor is designed based on the particle filter optimal prediction theory and the AR model time series analysis method. Because the influence of up and down motions on the vertical motion of the ideal landing point is the largest, the compensation effects of the designed predictor and compensator are simulated and verified based on the up and down motion of the power spectrum. For the compensation for the lateral motion, a tracking strategy of the horizontal measurement axis of the inertial stability coordinate system to the horizontal axis of the hull coordinate system (center line of the deck) is proposed. The tracking effects of the horizontal measurement axis of the designed integral and inertial tracking strategies are simulated and compared. Secondly, the lateral deck motion compensation commands are designed, and the compensation effects of different forms of compensation commands are verified by simulations. Finally, the compensation effects for the lateral deck motion under integral and inertial tracking strategies are simulated and analyzed.

Suggested Citation

  • Chen Cheng & Zian Wang & Zheng Gong & Pengcheng Cai & Chengxi Zhang, 2022. "Prediction and Compensation Model of Longitudinal and Lateral Deck Motion for Automatic Landing Guidance System," Mathematics, MDPI, vol. 10(19), pages 1-43, September.
    • Handle: RePEc:gam:jmathe:v:10:y:2022:i:19:p:3440-:d:921504
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    References listed on IDEAS

    as
    1. Hai-Xu Li & Fei-Yun Gao & Chu-Jun Hu & Qiang-Lin An & Xiu-Quan Peng & Yan-Ming Gong, 2021. "Trajectory Track for the Landing of Carrier Aircraft with the Forecast on the Aircraft Carrier Deck Motion," Mathematical Problems in Engineering, Hindawi, vol. 2021, pages 1-11, December.
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    Cited by:

    1. Zian Wang & Zheng Gong & Yang Yang & Yongzhen Liu & Pengcheng Cai & Chengxi Zhang, 2022. "Guidance Law for Autonomous Takeoff and Landing of Unmanned Helicopter on Mobile Platform Based on Asymmetric Tracking Differentiator," Mathematics, MDPI, vol. 11(1), pages 1-39, December.

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