Question
Write a Matlab function that computes the Cartesian position and velocity of a satellite on an orbit in the perifocal frame, given the gravitational parameter
Write a Matlab function that computes the Cartesian position and velocity of a satellite on an orbit in the perifocal frame, given the gravitational parameter (mu) , the semi-major axis a, the true anomaly, the eccentricity e, and the true anomaly (theta).
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Intelligent Information And Database Systems 12th Asian Conference ACIIDS 2020 Phuket Thailand March 23 26 2020 Proceedings
Authors: Pawel Sitek ,Marcin Pietranik ,Marek Krotkiewicz ,Chutimet Srinilta
1st Edition
9811533792, 978-9811533792
