TY  - RPRT
TI  - Numerical Computation of a Continuous-thrust State Transition Matrix Incorporating Accurate Hardware and Ephemeris Models
AU  - Ellison, Donald
AU  - Conway, Bruce
AU  - Englander, Jacob
PY  - 2015
UR  - https://ntrs.nasa.gov/citations/20150000799
ID  - 20150000799
ER  -