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
UR  - https://ntrs.nasa.gov/citations/20220013178
ID  - 20220013178
ER  -