Abstract
In this Paper, we proposed two new predictor corrector methods for solving Kepler's equation in hyperbolic case using quadrature formula which plays an important and significant rule in the evaluation of the integrals. The two procedures are developed that, in two or three iterations, solve the hyperbolic orbit equation in a very efficient manner, and to an accuracy that proves to be always better than 10^-15. The solution is examined with e ∈[1.5,6] and M_h∈ [0.5,6] with grid size ∆M_h=∆_e = 0.5, using the first guesses hyperbolic eccentric anomaly is H_o=In(2M_h/e + 1.5) and H_o=In(2M_h/e +2) , where e is the eccentricity and M_h is the hyperbolic mean anomaly.
Keywords
Hyperbolic trajectory, Hyperbolic eccentric anomaly, Quadrature rule, Predictor-corrector method.
Article Type
Article
How to Cite this Article
Rasheed, Mohammed S.
(2014)
"On Solving Hyperbolic Trajectory Using New Predictor-Corrector Quadrature Algorithms,"
Baghdad Science Journal: Vol. 11:
Iss.
1, Article 23.
DOI: https://doi.org/10.21123/bsj.2014.11.1.186-192
