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Remote Sensing System of Odometry and Telemetry data in Real- Time

机译:测距和遥测数据实时遥感系统

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The most important task in rocket launch especially in mini-satellite launch is transmission system the consist of sending and receiving data in real-time. Generally, remote sensing of mini satellite consists of several data such as Telemetry data, Odometry data and image data. Telemetry data contains values of air temperature, air pressure, wind direction and compass. The Odometry data contains altitude, latitude, longitude, Accelerometer, gyroscope or values related to Trajectory of payload rocket. One important system in remote sensing is the Ground Control Station (GCS) or Earth Station, this component is a control center that may be located on land or sea, this system provides facilities for control of motion or silent monitoring objects, this application holds a set of data visualized in the form of curves and graphs with two or three-dimensional animation models. This monitoring application is usually real-time and it is necessary because in mini satellite launch is impossible to control payload if the communication is not real time. Communications media used between payload rocket and Ground Control Station use cable or wireless transmission media. In the end, the results of monitoring can be used as a reference or can be reprocessed to get a conclusion.
机译:在火箭发射中,特别是在微型卫星发射中,最重要的任务是传输系统,该系统包括实时发送和接收数据。通常,小型卫星的遥感由遥测数据,里程计数据和图像数据等几种数据组成。遥测数据包含空气温度,气压,风向和指南针的值。里程表数据包含高度,纬度,经度,加速度计,陀螺仪或与有效载荷火箭的轨迹相关的值。遥感中的一个重要系统是地面控制站(GCS)或地球站,该组件是可能位于陆地或海洋上的控制中心,该系统提供了用于控制运动或静音监视对象的设施,该应用程序具有一组具有二维或三维动画模型的曲线和图形形式的可视化数据集。该监视应用程序通常是实时的,因此很有必要,因为在微型卫星发射中,如果通信不是实时的,则不可能控制有效载荷。有效载荷火箭与地面控制站之间使用的通信媒体使用电缆或无线传输媒体。最后,监测结果可以作为参考或可以重新处理以得出结论。

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