Digital image system for determining relative position and motio

Optics: measuring and testing – Angle measuring or angular axial alignment – Relative attitude indication along 3 axes with photodetection

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Details

2502061, 2502062, 348135, 3561415, 244171, G01B 1126, B64G 136

Patent

active

054933927

ABSTRACT:
The system includes a reflector assembly mounted on a first one of a pair of spacecraft. The reflector assembly includes a mirror around which are positioned a mirror and retroreflectors. A light source mounted on the second spacecraft illuminates the assembly the reflections from which are directed into a radiometer which is also mounted on the second spacecraft. The mirror has a known curvature, and the known curvature in conjunction with the retroreflectors allow calculation of the position and motion parameters of the first spacecraft relative to the second.

REFERENCES:
patent: 4815845 (1989-03-01), Colbaugh et al.
patent: 4834531 (1989-05-01), Ward
patent: 5119305 (1992-06-01), Ferro
patent: 5173750 (1992-12-01), Laukaitis
patent: 5207003 (1993-05-01), Yamada et al.

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