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The pointing system of the Herschel space observatory: Description, Calibration, Performance and improvements

机译:赫歇尔空间天文台的指向系统:说明,校准,性能和改进

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We present the activities carried out to calibrate and characterise the performance of the elements of attitude control and measurement on board the Herschel spacecraft. The main calibration parameters and the evolution of the indicators of the pointing performance are described, from the initial values derived from the observations carried out in the performance verification phase to those attained in the last year and half of mission, an absolute pointing error around or even below 1 arcsec, a spatial relative pointing error of some 1 arcsec and a pointing stability below 0.2 arsec. The actions carried out at the ground segment to improve the spacecraft pointing measurements are outlined. On-going and future developments towards a final refinement of the Herschel astrometry are also summarised. A brief description of the different components of the attitude control and measurement system (both in the space and in the ground segments) is also given for reference.We stress the importance of the cooperation between the different actors (scientists, flight dynamics and systems engineers, attitude control and measurement hardware designers, star-tracker manufacturers, etc.) to attain the final level of performance.
机译:我们介绍了在Herschel航天器上进行的用于校准和表征姿态控制和测量要素性能的活动。描述了主要的校准参数和指向性能指标的变化,从性能验证阶段的观测值得出的初始值,到上半年和任务的一半达到的初始值,均会出现大约或等于绝对误差。即使低于1 arcsec,空间相对指向误差约为1 arcsec,而指向稳定性低于0.2 arsec。概述了在地面部分进行的改善航天器指向测量的动作。还总结了为进一步完善Herschel天文测量技术而进行中的和未来的发展。还简要介绍了姿态控制和测量系统的不同组成部分(在空间和地面部分),以供参考。我们强调了不同参与者(科学家,飞行动力学和系统工程师)之间合作的重要性,姿态控制和测量硬件设计师,星跟踪器制造商等)以达到最终的性能水平。

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