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VARIATIONS IN THE TELEMETRY OF AN OFFEQ SATELLITE'S SUN SENSORS

机译:OFFEQ卫星太阳传感器遥测的变化

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One of the Israeli Offeq satellites has two fine solar aspect sensors which are analog devices based on a silicon quadrant detector. They exhibited variations in the telemetry since the beginning of mission that were similar for the four quadrants of the same detector. The telemetry signals of sun sensor no.1 declined ~14% and the signals of sun sensor no.2 declined ~10% during the first day of mission. The signals of sun sensor no.1 gradually stabilized at ~60% variation (~40% of the expected signals) while those of sun sensor no.2 stabilized at ~40% variation (~60% of the expected signals). Such values were sufficient for the normal continuous operation of the sensors. The angular difference of the sun vectors, calculated from the data of the two sensors, was small but a slight increase was observed from 0.2°-0.3° during the first days of mission to 0.4°-0.6° later. The goal of our investigation was to find out the possible causes for this behavior and suggest how to prevent them in future satellites. It included preliminary screening of all the possible causes, experimental and theoretical work done in order to support or exclude the remaining causes, conclusions and recommendations. The preliminary screening identified the most probable reasons for the telemetry variations as either the direct interaction of the optical window of the sun sensor with the space environment or its contamination. Our extensive computations and experiments indicated the importance of the contamination mechanisms but excluded direct interaction with the space environment as a major cause for the behavior. The most probable contamination sources were either outgassing from internal sources of the satellite and/or outgassing from one of the solar panels before their deployment. Partial fixation of the contaminants could occur by the combined effects of the space environment, especially by atomic oxygen and UV radiation. The conclusions led to recommendations for future missions.
机译:其中一个以色列OFFEQ卫星具有两个精细的太阳能方面传感器,它是基于硅象限探测器的模拟设备。它们在同一检测器的四次象限类似的使命开始以来,他们在遥测中表现出遥测的变化。太阳传感器No.1的遥测信号下降了〜14%,在使命的第一天下,Sun传感器的信号下降〜10%。 Sun传感器的信号No.1在〜60%的变化(〜40%的预期信号)逐渐稳定,而Sun传感器No.2稳定在〜40%的变异(预期信号的〜60%)。这种值足以用于传感器的正常连续操作。从两个传感器的数据计算的太阳载体的角度差异很小,但在任务的第一天期间从0.2°-0.3°观察到0.4°-0.6°的略微增加。我们调查的目标是找出这种行为可能的原因,并建议如何在未来的卫星中防止它们。它包括初步筛选所有可能的原因,实验和理论工作,以便支持或排除剩余的原因,结论和建议。初步筛选鉴定了遥测变化的最可能原因,作为太阳传感器的光学窗口与空间环境的直接相互作用或其污染。我们的广泛计算和实验表明了污染机制的重要性,但与空间环境中的直接互动作为行为的主要原因。最可能的污染源是从卫星的内部来源分配和/或在部署之前从一个太阳能电池板放水。污染物的部分固定可以通过空间环境的综合影响,尤其是由原子氧和紫外线辐射发生。结论导致了未来任务的建议。

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