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In-orbit verification, calibration, and performance of the Heliospheric Imager on the STEREO mission

机译:STEREO任务中日球成像仪的在轨验证,校准和性能

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摘要

The Heliospheric Imager (HI) forms part of the SECCHI suite of instruments aboard the two NASA STEREO spacecraft which were launched successfully from Cape Canaveral AFB on 25 Oct 2006 (26 Oct UTC). Following lunar swingby's on 15 Dec and 21 Jan respectively, the two spacecraft were placed in heliocentric orbits at approximately 1 AU - one leading and one lagging the Earth, with each spacecraft separating from the Earth by 22.5° per year. Each HI instrument comprises two wide-angle optical cameras - HI-1 and HI-2 have 20° and 70° fields-of-view which are off-pointed from the Sun direction by 14.0° and 53.7° respectively, with the optical axes pointed towards the ecliptic plane. In this way the cameras will for the first time provide stereographic images of the solar corona, and in particular of Coronal Mass Ejections (CMEs) as they propagate outwards through interplanetary space towards the Earth and beyond. The wide-field coverage of HI enables imaging of solar ejecta from 15 to about 330 solar radii whilst the other SECCHI instruments (2 coronagraphs and an EUV imager) provide coverage from the lower corona out to 15 solar radii. This paper briefly reviews the design and performance requirements for the instrument. The various activation, checkout and calibration activities before and after opening the instrument's protective cover or door (instrument 'first-light') are then described and it is shown that the instrument has met the design requirements, including CCD and camera imaging performance, correction for shutterless operation of the cameras, straylight rejection and thermal requirements. It is demonstrated from observations of a CME event on 24-25 Jan 2007 that the instrument is capable of detecting CMEs at an intensity of 1% of the coronal background. Lessons learnt during the design, development and in-orbit operation of the instrument are discussed.
机译:日射成像仪(HI)是两架NASA STEREO航天器上SECCHI仪器套件的一部分,该航天器于2006年10月25日(世界标准时间10月26日)从卡纳维拉尔角空军基地成功发射。在分别于12月15日和1月21日进行月球大摆之后,两架航天器被放置在日心说的轨道上,大约1 AU-一架领先于地球,另一架落后于地球,每架航天器每年与地球的距离为22.5°。每个HI仪器都包括两个广角光学相机-HI-1和HI-2的视场角分别为20°和70°,它们与太阳方向的偏角分别为14.0°和53.7°,光轴指向黄道平面。这样,当摄​​像机通过行星际空间向外传播并朝着地球及更远的方向传播时,它们将首次提供太阳日冕,尤其是日冕质量抛射(CME)的立体图像。 HI的宽视场覆盖范围使太阳射出的成像范围从15到大约330太阳半径,而其他SECCHI仪器(2幅电晕仪和EUV成像仪)提供了从较低电晕到15太阳半径的覆盖范围。本文简要回顾了该仪器的设计和性能要求。然后描述了在打开仪器的保护盖或门(仪表“第一灯”)之前和之后的各种激活,检查和校准活动,结果表明仪器已达到设计要求,包括CCD和照相机成像性能,校正用于摄像机的无快门操作,杂散光抑制和热要求。从2007年1月24日至25日对CME事件的观察中可以看出,该仪器能够检测到冠状背景的1%强度的CME。讨论了在仪器设计,开发和在轨操作过程中获得的经验教训。

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