TY  - RPRT
TI  - A method of testing attitude control systems during the development phase
AU  - Besonis, A.
AU  - Dougherty, H.
AU  - Levinthal, J.
AU  - Meadows, P.
PY  - 1981
UR  - https://ntrs.nasa.gov/citations/19810048487
ID  - 19810048487
ER  -