Paper
15 June 2006 Pointing and image stability for spaceborne sensors: from comet impactors to observations of extrasolar planets
Stephen E. Kendrick, Jeremy Stober, Ian Gravseth
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Abstract
From hitting a comet to long-term observations to find and characterize extrasolar planets, the spacecraft platform pointing accuracy and stability are fundamental. We describe the pointing requirements for Deep Impact, Kepler, and future extrasolar planet missions such as EPIC, and the approach to allow stable long-term measurements. The guidance, navigation, and control system consists of a suite of systems which can include star trackers, gyros, fine guidance sensors, reaction wheels, fast steering mirrors, and active and passive isolation features. One-fifth to one-twentieth of a pixel attitude determination may be needed with stabilities an order of magnitude tighter for observations that may last thousands of seconds. 1.5 milliarcsecond 3-sigma pointing stability can be achieved for the observatory enabling precision measurements by the scientific payloads.
© (2006) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Stephen E. Kendrick, Jeremy Stober, and Ian Gravseth "Pointing and image stability for spaceborne sensors: from comet impactors to observations of extrasolar planets", Proc. SPIE 6265, Space Telescopes and Instrumentation I: Optical, Infrared, and Millimeter, 62652V (15 June 2006); https://doi.org/10.1117/12.669068
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Cited by 4 scholarly publications.
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KEYWORDS
Stars

Sensors

Space operations

Control systems

Gyroscopes

Mirrors

Observatories

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