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DYNAMICAL BINNING FOR HIGH ANGULAR RATE STAR TRACKING

机译:高角速率星跟踪的动态装箱

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Recent advances in CCD and Active Pixel Sensor (APS) technology and the development of efficient star pattern recognition algorithms hold the prospect of realising a star tracker system that can serve as the only on-board attitude sensor. One of the obstacles to be overcome to attain this objective is the loss of performance of star trackers in the presence of high angular rates. Typically, accuracy degradation sets in at rates of 0.1-0.2 deg/s and most sensors have lost track at 1-1.5 deg/s. This is a severe limitation since angular velocities of up to 1 deg/s or higher are not uncommon on spacecraft. This paper describes a concept, called "dynamical binning", for enhancing the robustness of star trackers to high angular rates. Under dynamical conditions, the star image appears to be moving on the pixel array. The photon flux from the star is spread over a large number of pixels thus resulting in a low SNR. The proposed concept aims to de-spread the star image by oversampling and combining the pixel read-outs from successive subsamples in a manner that compensates for the motion of the star image. Dynamical binning is considered here in the context of APS-based star sensors. APSs are well-suited to this technique because they offer greater flexibility in the processing of pixel-level information and because the logic required for dynamical binning can be implemented directly on the same imager chip hosting the pixel array. After describing the dynamical binning algorithm, the paper presents the results of simulations that confirm the gains in SNR afforded by this technique. Implementation aspects are also discussed. In particular it is argued that on-chip implementation of the algorithm is feasible with current technology. Finally, plans for a prototype imager with dynamical binning to be realised in ESTEC are discussed. A patent application for the dynamical binning concept has been filed by ESA.
机译:CCD和有源像素传感器(APS)技术的最新进展以及有效的星形模式识别算法的发展,都有望实现一种可以用作唯一机载姿态传感器的星形跟踪器系统。要实现此目标需要克服的障碍之一是在高角速率下星跟踪仪的性能下降。通常,精度下降的速率为0.1-0.2度/秒,大多数传感器的跟踪速度为1-1.5度/秒。这是一个严重的限制,因为高达1度/秒或更高的角速度在航天器上并不罕见。本文介绍了一种称为“动态分箱”的概念,用于将恒星跟踪器的鲁棒性提高到高角速率。在动态条件下,星形图像似乎在像素阵列上移动。来自恒星的光子通量散布在大量像素上,从而导致低SNR。所提出的概念旨在通过对来自连续子样本的像素读数进行过采样和组合来对星图像进行解扩,以补偿星图像的运动。在基于APS的恒星传感器中考虑动态装仓。 APS非常适合此技术,因为它们在像素级信息的处理中提供了更大的灵活性,并且因为动态合并所需的逻辑可以直接在托管像素阵列的同一成像器芯片上实现。在描述了动态分箱算法之后,本文提出了仿真结果,该仿真结果证实了该技术所提供的SNR增益。还讨论了实现方面。特别是,有人认为,该算法的片上实现在当前技术下是可行的。最后,讨论了在ESTEC中实现具有动态装仓的原型成像仪的计划。 ESA已为动态分箱概念申请了专利。

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