TY  - RPRT
TI  - Spacecraft Attitude Control Using Nonlinear Servomechanism Theory
AU  - Huang, J.
AU  - Lin, C.
AU  - Hadaegh, F. Y.
AU  - Chiang, R. Y.
PY  - 1994
UR  - https://ntrs.nasa.gov/citations/20060037958
ID  - 20060037958
ER  -