Kepler's Equation is solved over the entire range of elliptic motion by a fifth-order refinement of the solution of a cubic equation. This method is not iterative, and requires only four transcendental function evaluations: a square root, a cube root, and two trigonometric functions. The maximum relative error of the algorithm is less than one part in 10(exp 18), exceeding the capability of double-precision computer arithmetic. Roundoff errors in double-precision implementation of the algorithm are addressed, and procedures to avoid them are developed
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICR...
Numerical methods are usually constructed for solving mathematical problems such as differential equ...
In this Paper, we proposed two new predictor corrector methods for solving Kepler's equation in hype...
A new approach for solving Kepler equation for elliptical orbits is developed in this paper. This ne...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for several highly de...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for several highly de...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for se...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for se...
Quadratic Newton-Raphson iteration techniques for numerical solutions of Keplers universal transcend...
Context. This paper introduces a new approach for solving the Kepler equation for hyperbolic orbits....
Context. This paper introduces a new approach for solving the Kepler equation for hyperbolic orbits....
We derive and present a fast and accurate solution of the initial value problem for Keplerian motion...
Context. Many algorithms to solve Kepler’s equations require the evaluation of trigonometric or root...
Financiado para publicación en acceso aberto: Universidade de Vigo/CISUGIn a recent MNRAS article, R...
Financiado para publicación en acceso aberto: Universidade de Vigo/CISUGIn a recent MNRAS article, R...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICR...
Numerical methods are usually constructed for solving mathematical problems such as differential equ...
In this Paper, we proposed two new predictor corrector methods for solving Kepler's equation in hype...
A new approach for solving Kepler equation for elliptical orbits is developed in this paper. This ne...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for several highly de...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for several highly de...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for se...
Context. The repetitive solution of Kepler’s equation (KE) is the slowest step for se...
Quadratic Newton-Raphson iteration techniques for numerical solutions of Keplers universal transcend...
Context. This paper introduces a new approach for solving the Kepler equation for hyperbolic orbits....
Context. This paper introduces a new approach for solving the Kepler equation for hyperbolic orbits....
We derive and present a fast and accurate solution of the initial value problem for Keplerian motion...
Context. Many algorithms to solve Kepler’s equations require the evaluation of trigonometric or root...
Financiado para publicación en acceso aberto: Universidade de Vigo/CISUGIn a recent MNRAS article, R...
Financiado para publicación en acceso aberto: Universidade de Vigo/CISUGIn a recent MNRAS article, R...
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.MICR...
Numerical methods are usually constructed for solving mathematical problems such as differential equ...
In this Paper, we proposed two new predictor corrector methods for solving Kepler's equation in hype...