结果表明，采用主动控制技术可大大降低起落架的冲击载荷和振动载荷，提高飞机的滑行性能。
It is shown that the impact loads and vibration loads can be greatly reduced by adopting optimal control techniques, and the taxiing performance of airplane can be greatly improved.
它的特点冲击主动振动控制，这大大减少了振动和增加用户的舒适性和生产力。
It features SHOCKS - Active vibration Control which significantly reduces vibration and increases user comfort and productivity.
它的特点冲击主动振动控制，这大大减少了振动和增加用户的舒适性和生产力。
It features SHOCKS - Active vibration Control which significantly reduces vibration and increases user comfort and productivity.
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