NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Three-Axis Attitude Control With a Single WheelSingle-device attitude-control system provides stabilization along three axes. Flywheel connected to electronically controlled motor rotates on magnetic bearing. At high rotational speed, small angular displacements about x and y axes, in response to control signals enable storage of relatively large amounts of angular momentum. Angular momentum about z axis stored in changes in rotational speed.
Document ID
19870000144
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Studer, P. A.
Date Acquired
August 13, 2013
Publication Date
March 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
GSC-12970
Accession Number
87B10144
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available