Abstract The Gauss-Jackson multi-step predictor-corrector method is widely used in numerical integration problems for astrodynamics and dynamical astronomy. The U.S. space surveillance centers have used an eighth-order Gauss-Jackson algorithm since the 1960s. In this paper, we explain the algorithm including a derivation from first principals and its relation to other multi-step integration methods. We also study its applicability to satellite orbits including its accuracy and stability.
Implementation of Gauss-Jackson Integration for Orbit Propagation
2004
Aufsatz (Zeitschrift)
Englisch
Implementation of Gauss-Jackson Integration for Orbit Propagation
Springer Verlag | 2004
|Implementation of Gauss-Jackson Integration for Orbit Propagation
Online Contents | 2004
|Implementation of Gauss-Jackson Integration for Orbit Propagation (AAS 01-426)
British Library Conference Proceedings | 2001
|Orbit Propagation Using Gauss-Legendre Collocation
British Library Conference Proceedings | 2012
|Orbit Propagation Using Gauss-Legendre Collocation
AIAA | 2012
|