Electronics Optics & Control, Volume. 22, Issue 9, 68(2015)

An H2 Preview Control Based Automatic Landing Control Method for Carrier Based Aircraft

SHAO Min-min, GONG Hua-jun, ZHEN Zi-yang, and JIANG Ju
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  • [in Chinese]
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    By taking carrier based aircraft as the studying object, we set up the dynamic model and design a carrier based aircraft automatic landing control system based on the H2 full information preview controller, which can suppress the interference caused by carrier air wake movement and track the landing glide slope. Taking a certain type of carrier based aircraft as the controlled object, a non linear numerical simulation is made. The results show that: 1) the H2 full information preview control strategy can improve the effect of rejecting air wake interference, obtain a quicker system response and a satisfactory trajectory tracking effect;and 2) the control effect is better than that of PID control.

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    SHAO Min-min, GONG Hua-jun, ZHEN Zi-yang, JIANG Ju. An H2 Preview Control Based Automatic Landing Control Method for Carrier Based Aircraft[J]. Electronics Optics & Control, 2015, 22(9): 68

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    Paper Information

    Received: Oct. 10, 2014

    Accepted: --

    Published Online: Jan. 28, 2021

    The Author Email:

    DOI:10. 3969/j. issn. 1671 一637x. 2015.09.015

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