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Special calibrations during AstroSat mission operations towards meeting observation and pointing requirements
Journal of Astrophysics and Astronomy ( IF 1.1 ) Pub Date : 2021-05-29 , DOI: 10.1007/s12036-021-09728-0
K. Subbarao , N. Hari Prasad Rao , V. Mahadevan , R. Pandiyan , J. S. Khoral

AstroSat, India’s first astronomical observatory was launched on 28th September 2015 by PSLV into an orbit of altitude 650 km and 6o inclination. The simultaneous observations made by the payloads allow imaging of celestial source in various wavebands and has resulted in scientific achievements published in various fora. AstroSat is designed to carry 6 (5 +1 auxiliary) astronomy payloads namely, UVIT, LAX-PC, SXT, CZTI, CPM and SSM. The payloads are mounted such that the boresight of all the 4 main payloads except SSM are along the +Roll direction in body frame. To meet all requirements of different payloads carried on-board AstroSat, various mission planning, analysis, and operations specific to this mission are carried out. These include post launch observations and mitigations planned and implemented onboard.



中文翻译:

在 AstroSat 任务操作期间进行特殊校准,以满足观测和指向要求

印度第一个天文台 AstroSat 于 2015 年 9 月 28 日由 PSLV 发射到海拔 650 公里、倾角 6 度的轨道上。有效载荷进行的同时观测允许对各种波段的天体进行成像,并已在各种论坛上发表了科学成果。AstroSat 旨在携带 6 个(5 +1 辅助)天文有效载荷,即 UVIT、LAX-PC、SXT、CZTI、CPM 和 SSM。有效载荷的安装使得除 SSM 外的所有 4 个主要有效载荷的视轴都沿着机身框架中的 + 滚动方向。为了满足 AstroSat 上携带的不同有效载荷的所有要求,针对该任务进行了各种任务规划、分析和操作。其中包括在船上计划和实施的发射后观察和缓解措施。

更新日期:2021-05-30
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