TY  - RPRT
TI  - Finite element method for optimal guidance of an advanced launch vehicle
AU  - Hodges, Dewey H.
AU  - Bless, Robert R.
AU  - Calise, Anthony J.
AU  - Leung, Martin
PY  - 1992
UR  - https://ntrs.nasa.gov/citations/19920057267
ID  - 19920057267
ER  -