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NASA NTRS ยท 19890000220

Alignment System For Docking Control

Abstract

Concept for alignment of vehicle approaching station based on generation of coherent, polarized light or microwave beam by station and measurement of beam propagation and polarization axes by vehicle. Intended for use in docking of spacecraft in flight and in robotics. Conical and corner-cube reflectors on vehicle disperse portions of incident light beam to sensors on vehicle and station, respectively. Station uses return signal for ranging and tracking. Known mathematical relationship among direction of beam and positions of reflected light on photodetector arrays used to calculate orientation of vehicle.

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BibTeXRIS

Iwasaki, Richard S.. 1989-05-01. Alignment System For Docking Control. https://ntrs.nasa.gov/citations/19890000220

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