TY  - RPRT
TI  - An ODE-Fitting Approach to Estimate Critical Aircraft Performance Parameters for Trajectory Prediction
AU  - Tejas G Puranik
AU  - Aida Sharif Rohani
AU  - Krishna M Kalyanam
PY  - 2022
UR  - https://ntrs.nasa.gov/citations/20220009339
ID  - 20220009339
ER  -