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Magnetic field cancellation techniques for the Mars Global Surveyor solar array

机译:火星全球测量师太阳能阵列的磁场取消技术

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The Mars Global Surveyor spacecraft carries a sensitive magnetometer system to detect and characterize the intrinsic magnetic field of Mars, if one exists. The use of booms to place the sensors remote from the spacecraft was not possible due to resource constraints. Instead, the sensors were mounted at the outer edge of the solar array, in close proximity to strings of solar cells. The current geometry in the array was optimized with a piecewise linear simulation to minimize the magnetic field generated at the sensor by the circulating currents under all operating conditions. A number of novel techniques were used in achieving magnetic field cancellation including carefully chosen circuit path lengths with zero area in selected strings, and sensitive magnetic verification tests in the Earth's field with a resolution of 1 part in 200000. The results show that the field generated by the array at the sensor location during the Mars mapping phase of the mission and under nominal conditions will be less than 0.4 to 0.6 nT (1nT=10/sup -5/ Gauss) under full solar illumination. The design is also reasonably tolerant of string failures. This major achievement would not have been possible without a close and synergistic interaction among the manufacturer, scientists and spacecraft engineers during the design, simulation and test of the solar array.
机译:火星全球测量师航天器带有一个敏感的磁力计系统,以检测和表征MARS的内在磁场,如果存在。由于资源约束,使用臂将远离航天器远离航天器的传感器。相反,传感器安装在太阳能阵列的外边缘,靠近太阳能电池的串。阵列中的电流几何形状用分段线性模拟进行了优化,以最小化在所有操作条件下通过循环电流在传感器处产生的磁场。使用许多新颖的技术在实现磁场消除中,包括仔细选择的电路路径长度,在200000年的分辨率为1部分的地球字段中具有零区域的尺寸区域,以及敏感的磁验证测试。结果表明该场产生的结果通过在MARS位置处的传感器位置处的阵列,任务的阶段,在全太阳能照射下,名义条件下的名称条件下的阶段小于0.4至0.6nt(1nt = 10 / sup -5 /高斯)。该设计也合理耐受弦故障。在设计,仿真和测试太阳能阵列期间,在制造商,科学家和航天器工程师之间没有紧密和协同互动,这一重大成就将无法实现。

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