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首页> 外文期刊>Journal of Mechatronics, Electrical Power, and Vehicular Technology >Vibration Disturbance Damping System Design to Protect Payload of the Rocket
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Vibration Disturbance Damping System Design to Protect Payload of the Rocket

机译:保护火箭有效载荷的减振阻尼系统设计

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Rocket motor generates vibrations acting on whole rocket body including its contents. Part of the body which is sensitive to disturbance is the rocket payload. The payload consists of various electronic instruments including: transmitter, various sensors, accelerometer, gyro, the embedded controller system, and others. This paper presents research on rocket vibration influence to the payload and the method to avoid disturbance. Avoiding influence of vibration disturbance can be done using silicone gel material whose typical damping factors are relatively high. The rocket vibration was simulated using electromagnetic motor, and the vibrations were measured using an accelerometer sensor. The measurement results were displayed in the form of curve, indicating the vibration level on some parts of the tested material. Some measurement results can be applied to determine the good material to attenuate vibration disturbance on the instruments of the payload.
机译:火箭发动机产生的振动作用于整个火箭体,包括其内含物。人体对干扰敏感的部分是火箭有效载荷。有效载荷由各种电​​子仪器组成,包括:发射器,各种传感器,加速度计,陀螺仪,嵌入式控制器系统等。本文研究了火箭振动对有效载荷的影响以及避免干扰的方法。可以使用典型阻尼系数相对较高的硅凝胶材料来避免振动干扰的影响。使用电磁电动机模拟火箭的振动,并使用加速度传感器测量振动。测量结果以曲线形式显示,表明被测材料某些部位的振动水平。某些测量结果可用于确定好的材料,以减轻有效载荷仪器上的振动干扰。

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