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Study on improving method about testing accuracy of the UAV pitch angle rate

机译:改进无人机校高角率测试精度的方法研究

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When the UAV is in Short period movement,it needs to increase longitudinal damping for keeping longitudinal stability. For flying stability, longitudinal damping controls tail wing according to longitudinal angle rate variety.For this reason,testing accuracy of longitudinal angle rate and taking a value of feedback coefficient is very important. Longitudinal angle rate is measured by velocity top in UAV.For the flexibility transforming of the UAV machine body structure,it will be severity influence to test accuracy of the UAV pitch angle rate.So it is important to do research on how to let up the influence and find out the measure.There is a wave point in the belly of the UAV machine body structure,in which move variety rate is zero.Making assurance the point and installing the sensor can reduce the influence in testing accuracy of the UAV pitch angle rate. By increasing filter wave link and choosing reasonable parameter,it will filter wave and clear up invalid number to judge feedback coefficient scope.
机译:当UAV处于短时间移动时,需要增加纵向阻尼以保持纵向稳定性。对于飞行稳定性,纵向阻尼根据纵向角度率的延伸尾翼。这是因为这个原因,测试纵向角率的准确性并采用反馈系数的值非常重要。纵向角度率是通过无人机的速度顶部测量的。对于UAV机器体结构的灵活性变换,它将严重影响,以测试UAV俯仰角率的准确性。所以对如何放弃研究是重要的影响和找出衡量标准。在UAV机器体结构的腹部有一个波点,其中MOVE多样性速率为零。占用保证点和安装传感器可以减少UAV俯仰角的测试精度的影响速度。通过增加滤波器波链路并选择合理参数,它将滤波波并清除无效号码以判断反馈系数范围。

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