将此方法运用到飞行器模拟训练系统中可有效地对该系统进行故障分析。

By using the method, it can effectively analyse the aerocraft Simulate Training System's failure.

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在搭建的一类C3I系统平台上，研究了系统的飞行器模拟器节点的特点及其功能。

The characteristics and functions of aerocraft simulator are studied based on a structured generic C3I system test-bed.

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在某飞行器模拟加载系统中，使用此方法进行转动惯量的测量和多余力的消除，取得了较为理想的结果，对电动加载系统的进一步研究具有参考价值。

The elimination of plus torque in electric loading system is resolved well by this method, and it has referenced value to thorough research in electric l...

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