介绍一种基于决策控制的半主动起落架减震器控制系统的动力学参数测量系统。
A dynamic parameter measurement system for absorber of undercarriage based on decision-making control is presented.
起落架在地面支撑飞机，油气式减震器吸收滑行和降落的负载。
The L/G support the aircraft on the ground and oil-pneumatic shock absorbers absorb taxi and landing loads.
A320起落架在地面支撑飞机，包括着陆减震器。
The A320 Landing Gear supports the aircraft on the ground and includes shock absorbers for landing.
全部三个起落架单元安装双腔油气减震器。
All three units of the gear are equipped oleo pneumatic shock absorbers.
负载反应单元(9)可连接在臂(4)的前端和减震器支柱的上部分(2)之间，使起落架用作半摇臂式起落架。
The load reacting unit (9) may be connected between a forward end of the arm (4) and the upper portion (2) of the shock absorber strut to make the gear act as a semi-levered landing gear.
负载反应单元(9)可连接在臂(4)的前端和减震器支柱的上部分(2)之间，使起落架用作半摇臂式起落架。
The load reacting unit (9) may be connected between a forward end of the arm (4) and the upper portion (2) of the shock absorber strut to make the gear act as a semi-levered landing gear.
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