The research on the scheme of Landing Guidance System based on electro-optical sensors is carried on first.

本文研究了基于光电成像的着陆引导系统方案。

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This paper introduced the principle of the automatic carrier landing guidance system and its filtering problem.

介绍了自动着舰导引系统的工作原理及其滤波问题。

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So active disturbance rejection controller (ADRC) was used to design the longitudinal carrier landing guidance system.

因此，采用自抗扰控制器(adrc)设计了纵向着舰导引系统。

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Assessing the accuracy of guidance system, especially controlling of missile's attitude and station keeping maneuver and landing point forecasting all rely on the reliable trajectory measurement.

飞行器制导精度评估，特别是航天器的姿态与定点控制、落点预报等，都离不开高精度的外弹道测量数据。

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Assessing the accuracy of guidance system, especially controlling of missile's attitude and station keeping maneuver and landing point forecasting all rely on the reliable trajectory measurement.

飞行器制导精度评估，特别是航天器的姿态与定点控制、落点预报等，都离不开高精度的外弹道测量数据。

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