PERFORMANCE EVALUATION FOR POINTING CONTROL SYSTEM OF THE BALLOON-BORNE TELESCOPE

被引：0
|
作者：
Nakano, T. [1 ]
Fujimura, R. [1 ]
Sakamoto, Y. [1 ]
Yoshida, K. [1 ]
Kuwahara, T. [1 ]
Shoji, Y.
Taguchi, M.
Yamamoto, M.
Takahashi, Y.
机构：
[1] Tohoku Univ, Dept Aerosp, Aoba Ku, Sendai, Miyagi 9808579, Japan
来源：
SPACE FOR OUR FUTURE | 2013年 / 146卷
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The balloon-borne telescope is a planetary observation method launching a telescope to the altitude of more than 30 km by a stratospheric balloon. To conduct the long duration observation, the flight gondola has to equip with a pointing control system in order to catch and keep the target star in the field of view of the telescope during the flight. This research aims to develop the high accuracy pointing control system and conduct the technology demonstration flight. The goal of the pointing control is set as 0.1 arcsec. This paper introduces the results of the ground test and simulation study to evaluate the performance of the pointing control system.
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页码：381 / 391
页数：11
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