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Image stabilization system on SOLAR-B Solar Optical Telescope

机译:太阳能-B太阳能光学望远镜的图像稳定系统

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Extremely stable pointing of the telescope is required for images on the CCD cameras to accurately measure the nature of magnetic field on the sun. An image stabilization system is installed to the Solar Optical Telescope onboard SOLAR-B, which stabilizes images on the focal plane CCD detectors in the frequency range lower than about 20Hz. The system consists of a correlation tracker and a piezo-based tip-tilt mirror with servo control electronics. The correlation tracker is a high speed CCD camera with a correlation algorithm on the flight computer, producing a pointing error from series of solar granule images. Servo control electronics drives three piezo actuators in the tip-tilt mirror. A unique function in the servo control electronics can put sine wave form signals in the servo loop, allowing us to diagnose the transfer function of the servo loop even on orbit. The image stabilization system has been jointly developed by collaboration of National Astronomical Observatory of Japan/Mitsubishi Electronic Corp. and Lockheed Martin Advanced Technology Center Solar and Astrophysics Laboratory. Flight model was fabricated in summer 2003, and we measured the system performance of the flight model on a laboratory environment in September 2003, confirming that the servo stability within 0-20 Hz bandwidth is 0.001-0.002 arcsec rms level on the sun.
机译:CCD摄像机上的图像需要极其稳定的指向望远镜,以准确测量磁场上阳光下的磁场的性质。图像稳定系统安装在太阳能光学望远镜上的太阳能光学望远镜-B,其在低于约20Hz的频率范围内稳定在焦平面CCD检测器上的图像。该系统由带有伺服控制电子设备的相关跟踪器和基于压电的尖端倾斜镜组成。相关跟踪器是一种高速CCD摄像机,在飞行计算机上具有相关算法,从一系列太阳能颗粒图像产生指向误差。伺服控制电子设备驱动尖端倾斜镜中的三个压电致动器。伺服控制电子设备中的独特功能可以将正弦波形状的信号放在伺服循环中,允许我们诊断伺服循环的传递函数即使在轨道上也会。图像稳定系统是通过日本国家天文天文台的合作共同开发的,MITSUBISHI电子公司和洛克希德马丁先进技术中心太阳能和天体物理实验室。飞行模型在2003年夏季制作,我们于2003年9月在实验室环境中测量了飞行模式的系统性能,确认0-20 Hz带宽内的伺服稳定性在阳光下为0.001-0.002 arcsec rms水平。

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