Orbit equations with a set of conservative and a set of nonconservative perturbing potentials were considered. Scheifele's DS formulation of these equations has dependent variables similar to Delaunay's orbital elements with the true anomaly as the independent variable. Efficiency curves of computing cost v.s. accuracy were constructed for Adams integrators of order of 2 through 15 with several correcting algorithms and for a Runga-Kutta integrator. Considering stability regions, choices were made for the optimally efficient integration modes for the DS elements. Integrating in these modes reduces computing costs for a specified accuracy
A general time element, valid with any arbitrary independent variables, and used with Cartesian coor...
Study compares the use of five different methods for the computer solution of the restricted three-b...
Earth satellite orbit computations - Diliberto general perturbation method application in improved c...
Local error control for optimization of numerical integration orbit calculation technique
Local error control concept effect on optimization of orbital integration by multistep proces
Methods for analyzing the stability of satellites are discussed. The subjects considered are: (1) ti...
This paper focuses on the Gauss-Jackson algorithm for numerical integration, which particularly suit...
Computational and analytical techniques which simplify the solution of complex problems in orbit mec...
In this paper the fixed step Gauss-Jackson method is compared to two variable step integrators. The...
Multirevolution predictor-corrector algorithm applicability to numerical integration of orbit
A new class of linear multistep methods for numerical integration of differential equations is repor...
Two general purpose numerical integration schemes were built into the NASA-JSC computer system. The ...
Calculation of path deviation of satellite from reference trajectory - perturbation theor
Comparison of fourth order Runge-Kutta numerical integration technique with two numerical integratio...
AbstractComputer algebra systems are developing very fast and it is now possible to use new computat...
A general time element, valid with any arbitrary independent variables, and used with Cartesian coor...
Study compares the use of five different methods for the computer solution of the restricted three-b...
Earth satellite orbit computations - Diliberto general perturbation method application in improved c...
Local error control for optimization of numerical integration orbit calculation technique
Local error control concept effect on optimization of orbital integration by multistep proces
Methods for analyzing the stability of satellites are discussed. The subjects considered are: (1) ti...
This paper focuses on the Gauss-Jackson algorithm for numerical integration, which particularly suit...
Computational and analytical techniques which simplify the solution of complex problems in orbit mec...
In this paper the fixed step Gauss-Jackson method is compared to two variable step integrators. The...
Multirevolution predictor-corrector algorithm applicability to numerical integration of orbit
A new class of linear multistep methods for numerical integration of differential equations is repor...
Two general purpose numerical integration schemes were built into the NASA-JSC computer system. The ...
Calculation of path deviation of satellite from reference trajectory - perturbation theor
Comparison of fourth order Runge-Kutta numerical integration technique with two numerical integratio...
AbstractComputer algebra systems are developing very fast and it is now possible to use new computat...
A general time element, valid with any arbitrary independent variables, and used with Cartesian coor...
Study compares the use of five different methods for the computer solution of the restricted three-b...
Earth satellite orbit computations - Diliberto general perturbation method application in improved c...