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Aircraft System for Measuring the Angular Deflections of Control Surfaces

机译:用于测量控制面角向变形的飞机系统

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摘要

We consider the aircraft system hardware and software to measure the angular deflections of control surfaces. The experimental studies of a photoelectric transducer for converting the control surface angular deflections into digital codes are performed. The mathematical models are obtained to describe a dependence of measuring errors on the coordinates of emitter arrangement. The optimal emitter arrangement is determined using the mathematical models and a pilot model of the aircraft system proposed has been developed.
机译:我们考虑了飞机系统的硬件和软件来测量控制面的角偏转。进行了用于将控制面角偏转转换为数字代码的光电换能器的实验研究。获得数学模型以描述测量误差对发射器布置的坐标的依赖性。使用数学模型确定最佳发射器布置,并已开发出建议的飞机系统的飞行员模型。

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