TY  - RPRT
TI  - A new concept of stability in orbit propagation, useful for quantifying numerical errors
AU  - Pelaez, Jesus
AU  - Urrutxua, Hodei
AU  - Roa, Javier
PY  - 2017
UR  - https://ntrs.nasa.gov/citations/20210007659
ID  - 20210007659
ER  -