TY  - RPRT
TI  - Flexible body stability analysis of Space Shuttle ascent flight control system by using lambda matrix solution techniques
AU  - Bown, R. L.
AU  - Christofferson, A.
AU  - Lardas, M.
AU  - Flanders, H.
PY  - 1980
UR  - https://ntrs.nasa.gov/citations/19800061736
ID  - 19800061736
ER  -