The MAVEN Magnetic Field Investigation

磁强计 航天器 磁场 太阳风 火星探测计划 物理 磁通门罗盘 航空航天工程 仪表(计算机编程) 地球磁场 遥感 电气工程 计算机科学 工程类 地质学 天体生物学 量子力学 操作系统
作者
J. E. P. Connerney,J. R. Espley,P. Lawton,Simon J. Murphy,J. Odom,R. J. Oliversen,D. Sheppard
出处
期刊:Space Science Reviews [Springer Science+Business Media]
卷期号:195 (1-4): 257-291 被引量:346
标识
DOI:10.1007/s11214-015-0169-4
摘要

The MAVEN magnetic field investigation is part of a comprehensive particles and fields subsystem that will measure the magnetic and electric fields and plasma environment of Mars and its interaction with the solar wind. The magnetic field instrumentation consists of two independent tri-axial fluxgate magnetometer sensors, remotely mounted at the outer extremity of the two solar arrays on small extensions (“boomlets”). The sensors are controlled by independent and functionally identical electronics assemblies that are integrated within the particles and fields subsystem and draw their power from redundant power supplies within that system. Each magnetometer measures the ambient vector magnetic field over a wide dynamic range (to 65,536 nT per axis) with a resolution of 0.008 nT in the most sensitive dynamic range and an accuracy of better than 0.05 %. Both magnetometers sample the ambient magnetic field at an intrinsic sample rate of 32 vector samples per second. Telemetry is transferred from each magnetometer to the particles and fields package once per second and subsequently passed to the spacecraft after some reformatting. The magnetic field data volume may be reduced by averaging and decimation, when necessary to meet telemetry allocations, and application of data compression, utilizing a lossless 8-bit differencing scheme. The MAVEN magnetic field experiment may be reconfigured in flight to meet unanticipated needs and is fully hardware redundant. A spacecraft magnetic control program was implemented to provide a magnetically clean environment for the magnetic sensors and the MAVEN mission plan provides for occasional spacecraft maneuvers—multiple rotations about the spacecraft $x$ and $z$ axes—to characterize spacecraft fields and/or instrument offsets in flight.
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