• 使飞行器主动段很快地进入理想弹道上,系统采用非线性推力向量控制预测制导方法。

    In order to enter into the ideal trajectory with minimal energy, the nonlinear thrust vector control and the prediction guidance are adopted in the missile guidance control system.

    youdao

  • 使飞行器主动段很快地进入理想弹道上,系统采用非线性推力向量控制预测制导方法。

    In order to enter into the ideal trajectory with minimal energy, the nonlinear thrust vector control and the prediction guidance are adopted in the missile guidance control system.

    youdao

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