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用于直接系外行星成像的毫角秒指向系统的飞行演示。

Flight demonstration of a milliarcsecond pointing system for direct exoplanet imaging.

作者信息

Mendillo Christopher B, Chakrabarti Supriya, Cook Timothy A, Hicks Brian A, Lane Benjamin F

机构信息

Astronomy Department, Boston University, Boston, Massachusetts 02215, USA.

出版信息

Appl Opt. 2012 Oct 10;51(29):7069-79. doi: 10.1364/AO.51.007069.

Abstract

We present flight results from the optical pointing control system onboard the Planetary Imaging Concept Testbed Using a Rocket Experiment (PICTURE) sounding rocket. PICTURE (NASA mission number: 36.225 UG) was launched on 8 October 2011, from White Sands Missile Range. It attempted to directly image the exozodiacal dust disk of ϵ Eridani (K2V, 3.22 pc) down to an inner radius of 1.5 AU using a visible nulling coronagraph. The rocket attitude control system (ACS) provided 627 milliarcsecond (mas) RMS body pointing (~2'' peak-to-valley). The PICTURE fine pointing system (FPS) successfully stabilized the telescope beam to 5.1 mas (0.02λ/D) RMS using an angle tracker camera and fast steering mirror. This level of pointing stability is comparable to that of the Hubble Space Telescope. We present the hardware design of the FPS, a description of the limiting noise sources and a power spectral density analysis of the FPS and rocket ACS in-flight performance.

摘要

我们展示了搭载在行星成像概念试验台利用火箭实验(PICTURE)探空火箭上的光学指向控制系统的飞行结果。PICTURE(美国国家航空航天局任务编号:36.225 UG)于2011年10月8日从白沙导弹靶场发射。它试图使用可见光消零日冕仪直接对波江座ε星(K2V,3.22秒差距)的黄道外尘埃盘进行成像,直至其1.5天文单位的内半径。火箭姿态控制系统(ACS)提供了627毫角秒(mas)的均方根值机身指向(峰谷值约为2'')。PICTURE精细指向系统(FPS)使用角度跟踪相机和快速转向镜成功地将望远镜光束稳定到5.1 mas(0.02λ/D)的均方根值。这种指向稳定性水平与哈勃太空望远镜相当。我们展示了FPS的硬件设计、对限制噪声源的描述以及FPS和火箭ACS飞行性能的功率谱密度分析。

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