Modification of Three Order Methods For Solving Satellite Orbital Equation in Elliptical Motion
Modification of Three Order Methods For Solving Satellite Orbital Equation in Elliptical Motion

Mohammed S. Rasheed

Volume 14, Issue 1 , April 2020, , Page 33-37

https://doi.org/10.37652/juaps.2022.172315

Abstract
  In the present study, a modification for iterative methods of three order is presented by means of mean anomaly to calculate the values of E and e (true anomaly and eccentricity) respectively, ...  Read More ...