火卫一飞掠时MARSIS雷达回波的数值计算

D. Plettemeier, R. Hahnel, S. Hegler, A. Safaeinili, J. Plaut, B. Gaskell, R. Orosei, A. Cicchetti, G. Picardi
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引用次数: 8

摘要

火星探测器上的火星地下和电离层探测高级雷达(MARSIS)是迄今为止第一个也是唯一一个观测火星卫星火卫一的太空雷达。雷达回波测量了不同的飞掠轨迹。对火卫一地壳进行低频探测的主要目的是为了证明深层探测的可行性。本文提出了一种能够精确计算大型目标表面后向散射雷达回波的数值方法。该软件结合了雷达目标表面散射的物理光学计算和计算整个星载雷达系统辐射方向图的矩量法方法,其中频率相关辐射方向图的计算考虑了航天器上所有相关的增益变化和耦合效应。本文对仿真技术进行了说明,并对不同轨道的仿真结果进行了比较,对后向散射信号进行了解释。
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Numerical computation of radar echoes measured by MARSIS during phobos flybys
The Mars Advanced Radar for Subsurface and Ionosphere Sounding, “MARSIS”, on board MarsExpress is the first and so far only space borne radar that observed the Martian moon Phobos. Radar echoes were measured for different flyby trajectories. The primary aim of the low frequency sounding of the crust of Phobos is to prove the feasibility of deep sounding. In this paper we present a numerical method that allows precise computation of radar echoes backscattered from the surface of large objects. The software is based on a combination of a Physical Optics calculation of surface scattering of the radar target, and a Method of Moments approach to calculate the radiation pattern of the whole space borne radar system, whereby the calculation of the frequency dependent radiation pattern takes into account all relevant gain variations and coupling effects aboard the space craft. This paper explains the simulation techniques and presents a comparison of simulation results for different orbits, and an interpretation of the backscattered signals.
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