Aircraft actuator system failure can be detected by analytic redundancy analysis.
飞机舵机系统的机械故障可用解析余度法检测。
The invention provides an actuator system comprising an actuator member having first and second positions.
本发明提供了一种致动系统，包括具有第一位置和第二位置的致动器元件。
The experimental results show that this actuator system can not only be used as a fine feeder in mirror turning…
结果表明，该机构系统不仅适用于镜面车削时作精密微量进刀，而且还可以应用在误差动态补偿系统中作执行机构。
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