Motion of artificial satellites in the set of Eulerian redundant parameters. II

Details Motion of artificial satellites in the set of Eulerian redundant parameters. II Motion of artificial satellites in the set of Eulerian redundant parameters. II

Dec 1991

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1991em%26p...55..223s&link_type=abstract

Earth, Moon, and Planets (ISSN 0167-9295), vol. 55, Dec. 1991, p. 223-231.

Statistics

Applications

1

Ballistic Missiles, Power Series, Redundancy Encoding, Satellite Perturbation, Spacecraft Motion, Euler Equations Of Motion, Recursive Functions

Scientific paper

The full recurrent power-series solution is established for J2-gravity-perturbed motion in terms of the Eulerian redundant parameters. Applications of the method to the problem of the final state prediction are illustrated with numerical examples of some typical ballistic missiles, and a final state of very high accuracy is obtained for each case study.

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