TY  - RPRT
TI  - A Time-Regularized, Multiple Gravity-Assist Low-Thrust, Bounded-Impulse Model for Trajectory Optimization
AU  - Ellison, Donald H.
AU  - Englander, Jacob A.
AU  - Conway, Bruce A.
PY  - 2017
UR  - https://ntrs.nasa.gov/citations/20170001427
ID  - 20170001427
ER  -