Search NASA⌕ Search

NASA NTRS · 19690065256

Satellite attitude control using a torqued, 2-axis-gimbaled boom as the actuator.

Abstract

Torqued two axis gimbaled boom actuator satellite attitude control

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Buckingham, A. G., Gatlin, J. A., Pleasants, W. H.. 1969-09-01. Satellite attitude control using a torqued, 2-axis-gimbaled boom as the actuator.. https://ntrs.nasa.gov/citations/19690065256

Cite the original work for its findings. Save a collection to share your selection of sources.