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NASA NTRS · 19910052923

A quadrant-CCD star tracker

Abstract

The characteristics of a quadrant-CCD designed for pointing and tracking are discussed with reference to its use in an adaptive optics program. The quadrant-CCD is used to correct stellar image motion proceeding from atmospheric turbulence by means of a system in which a sensor measures the image offset and sends data to a high-speed tip/tilt mirror. The design and control of the device are detailed, including four 100-micron-square pixels, the quadrant architecture, controller electronics, and data acquisition computer and interface. The transfer function is set forth in the x and y directions, and transfer curves are shown. A laboratory simulation of random image motion was conducted to evaluate the performance of the quadrant-CCD as an image motion sensor, and the experimental results are presented. The suitability of the quadrant-CCD for space-based pointing and tracking uses is demonstrated by this test and two earlier theoretical studies. Some future developments which improve performance capabilities are mentioned.

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BibTeXRIS

Clampin, M., Durrance, S. T., Barkhouser, R., Golimowski, D. A., Wald, A., Fastie, W. G., Heidtmann, D. L., Blouke, Morley M., Westphal, James A., Janesick, James R.. 1990-01-01. A quadrant-CCD star tracker. https://ntrs.nasa.gov/citations/19910052923

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