Combining optimal control and self-tuning control theory, the adaptive control strategy for semi-active landing gear is proposed.

结合最优控制和自校正控制理论，给出了半主动起落架的自适应控制策略。

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The semi-active control landing gear model was simulated trough the Simulation soft MATLAB and the simulation results were in contrast with the results of passive control model.

以MATLAB软件为平台对半主动控制下的起落架着陆过程进行仿真，并与被动控制下的仿真结果作了分析对比。

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In general, the control methods of the aircraft 's landing gear shock absorbers are classified three categories: a passive type, an active type, and semi - active type.

一般地说，飞机起落架缓冲系统的控制方式有三种：被动控制、主动控制和半主动控制。

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