NASA NTRS · 20060037958
Spacecraft Attitude Control Using Nonlinear Servomechanism Theory
Abstract
The recently developed nonlinear servomechanism theory is applied to the attitude control of large maneuvering spacecraft subject to sinusoidal disturbances and parametric uncertainties.
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Huang, J., Lin, C., Hadaegh, F. Y., Chiang, R. Y.. 1994-04-01. Spacecraft Attitude Control Using Nonlinear Servomechanism Theory. https://ntrs.nasa.gov/citations/20060037958
Cite the original work for its findings. Save a collection to share your selection of sources.