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In-orbit verification system and method for satellite communication subsystem

机译:卫星通信子系统的在轨验证系统和方法

摘要

The present invention relates to satellite systems, and more particularly, to providing new systems and methods for verifying in-orbit performance and operation of satellite communications subsystems. In contrast to conventional payload IOT (in-orbit test), the present invention operates without uplink signals by generating hardware specific signatures using internally generated isolated thermal noise To do. This noise has been found to provide a very stable and repeatable signal for testing. Prior to launch, a repeater command sequence is executed to generate a hardware specific signature based on internally generated noise. The same repeater command sequence is executed in the trajectory to determine if the hardware specific signature has changed. The two signatures can be recorded and compared using a simple tool such as a spectrum analyzer. The method also includes the new use of the sun as a test signal source for calibrating the device, quantifying atmospheric effects, and using it as an intermediate reference power level during measurements. [Selection] Figure 10
机译:本发明涉及卫星系统,更具体地说,涉及提供用于检验卫星通信子系统的在轨性能和操作的新系统和方法。与传统的有效载荷IOT(在轨测试)相反,本发明通过使用内部产生的隔离热噪声To do产生硬件专用签名来在没有上行链路信号的情况下进行操作。已经发现该噪声为测试提供了非常稳定且可重复的信号。在启动之前,将执行转发器命令序列以基于内部生成的噪声来生成硬件特定的签名。在该轨迹中执行相同的转发器命令序列,以确定硬件特定的签名是否已更改。可以使用简单的工具(例如频谱分析仪)记录并比较两个签名。该方法还包括新使用太阳作为测试信号源,用于校准设备,量化大气影响并将其用作测量期间的中间参考功率水平。 [选择]图10

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