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NASA NTRS · 19910042196

Structural control sensors for CASES

Abstract

The Remote Attitude Measurement Sensor (RAMS) is currently baselined to meet two important sensor needs for CASES (Control, Astrophysics and Structures Experiment in Space). First, as a tip displacement sensor, RAMS is designed to provide accurate knowledge of the position and orientation of the boom tip assembly. Secondly, as a boom motion tracker, it is designed to monitor 43 reflective targets which are distributed along the length of the boom and provide displacment information for post facto processing. The design and operation of RAMS as these two types of sesnors are described, and attention is given to how RAMS interfaces with the CASES closed-loop control system and how systems identification is accommodated.

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BibTeXRIS

Davis, Hugh W., Sharkey, John P., Carrington, Connie K.. 1990-01-01. Structural control sensors for CASES. https://ntrs.nasa.gov/citations/19910042196

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