Orbital Equation Smoothing based Trajectory and Impact Point Prediction
Author:
Affiliation:
1. Jiuquan Satellite Launch Center, Company, China
Publisher
ACM
Link
https://dl.acm.org/doi/pdf/10.1145/3564858.3564862
Reference12 articles.
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4. Saleem Z . Extended Kalman filter for optimal determination of position, velocity and time of Earth orbiting satellites using carrier phase measurements from GNSS constellations[J] . 2011 . Saleem Z . Extended Kalman filter for optimal determination of position, velocity and time of Earth orbiting satellites using carrier phase measurements from GNSS constellations[J]. 2011.
5. Vamos C Craciun M . Polynomial Fitting[J]. 2012. Vamos C Craciun M . Polynomial Fitting[J]. 2012.
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