首页> 外文会议>2010 International Conference on Communications, Circuits and Systems >Analysis and compensation of errors of precalculated satellite overpass time and aircraft navigation system in spaceborne/airborne hybrid bistatic SAR
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Analysis and compensation of errors of precalculated satellite overpass time and aircraft navigation system in spaceborne/airborne hybrid bistatic SAR

机译:星载/机载混合双基地SAR中预先计算的卫星越区时间和飞机导航系统的误差分析与补偿

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The impact of errors of the precalculated satellite overpass time and aircraft navigation system on some performance parameters, i.e. the footprint overlapping time, the scene extension in azimuth, the offset of the imaging scene, in spaceborne/airborne hybrid bistatic SAR (SA-BSAR) is analyzed. Several related formulae are derived and simulations were performed using parameters of TerraSAR-X as the transmitter and PAMIR as the receiver. The results indicate that predication error of only 0.01 second for the satellite overpass time would cause the scene extension in azimuth to decrease 20 percent when the aircraft navigation system error reaches 5 seconds (the maximum possible value in normal case). Under the same prerequisite predication error of 0.28 second for the satellite overpass time would miss the chance to getting overlapped. A compensation method is proposed based on the idea that the radar satellite starts the beam steering just at the instant when it passes its ideal position rather than at the precalculated instant to begin steering. To accomplish this goal a far more precise prediction for the satellite overpass time must be made on the aircraft several seconds before the satellite's arrival. The concrete requirement for the prediction accuracy is derived. The required accuracy must be guaranteed to achieve the expected scene extension in azimuth.
机译:预计算的卫星越区时间和飞机导航系统的误差对一些性能参数的影响,例如,星载/机载混合双基地SAR(SA-BSAR)中的足迹重叠时间,方位的场景扩展,成像场景的偏移被分析。推导了几个相关的公式,并使用TerraSAR-X作为发送器和PAMIR作为接收器的参数进行了仿真。结果表明,当飞机导航系统误差达到5秒(正常情况下的最大可能值)时,卫星越过时间的预测误差只有0.01秒,将导致方位角的场景扩展减少20%。在相同的前提条件下,卫星越过时间的预测误差为0.28秒,将错过重叠的机会。基于这样一种思想,提出了一种补偿方法:雷达卫星仅在其经过理想位置的那一刻开始波束转向,而不是在预先计算的瞬间开始波束转向。为了实现这一目标,必须在飞机到达卫星几秒钟之前,对飞机的卫星越过时间做出更精确的预测。得出了对预测精度的具体要求。必须保证所需的精度,以实现预期的方位角场景扩展。

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