Paper
3 May 2007 Hydra AR&D sensor suite
Author Affiliations +
Abstract
AOS is designing a modular AR&D System named Hydra® and building an initial prototype with selected (near-field and docking) capabilities and expansion capabilities to accommodate a time-of-flight and far-field sensor. Lessons learned from DART and Orbital Express have been applied to the proposed Hydra® design. The prototype Hydra® system design includes an AVGS sensor head and an ULTOR® sensor head. Although the initial Hydra® system is a ground demonstration unit, design methods and component selection provide a straightforward path for building a space-qualified Hydra® system. The basic architectural component for Hydra® is based on a common processing platform that can be configured to process inputs from a variety of sensors. The design consists of three elements: The sensor head or camera, which can be mounted external to the spacecraft; the processing electronics, which can be mounted internal to the spacecraft; and the Hydra® target, which is mounted on the target spacecraft at or near the docking interface.
© (2007) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Fred Roe and Stephen R. Granade "Hydra AR&D sensor suite", Proc. SPIE 6555, Sensors and Systems for Space Applications, 65550H (3 May 2007); https://doi.org/10.1117/12.719328
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KEYWORDS
Sensors

Head

Space operations

Electronics

Prototyping

Cameras

Adaptive optics

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