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NASA NTRS ยท 19870000144

Three-Axis Attitude Control With a Single Wheel

Abstract

Single-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.

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BibTeXRIS

Studer, P. A.. 1987-03-01. Three-Axis Attitude Control With a Single Wheel. https://ntrs.nasa.gov/citations/19870000144

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