As an example, an OH-58A helicopter is introduced in the study, and the possible reduction in height-velocity restrictions is discussed using optimal control techniques.

最后，以OH-58A轻型直升机为例进行了算例分析，并且探讨了采用最优操纵方式缩小高度—速度回避区范围的可能性。

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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.

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。

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