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Structural control sensors for CASESThe 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.
Document ID
19910042196
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davis, Hugh W.
(Ball Aerospace Systems Group Boulder, CO, United States)
Sharkey, John P.
(Ball Aerospace Systems Div. Boulder, CO, United States)
Carrington, Connie K.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Spacecraft Instrumentation
Report/Patent Number
AAS PAPER 90-044
Meeting Information
Meeting: Annual Rocky Mountain Guidance and Control Conference
Location: Keystone, CO
Country: United States
Start Date: February 3, 1990
End Date: February 7, 1990
Sponsors: AAS
Accession Number
91A26819
Distribution Limits
Public
Copyright
Other

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