PG-EAM - Graduate Program in Aeronautical and Mechanical Engineering
PT EN
Article 1989

Earth oblateness effect on the optimal impulsive transfer between close orbits Part 2: Singular solutions

Acta Astronautica , vol. 19 , no. 5 , pp. 393-399

ISSN: 00945765

1
Citations
1
Authors

Abstract

This paper deals with the study of the singular solutions of optimal impulsive transfer problem between close quasi-circular-equatorial orbits, considering the Earth oblateness. These solutions are similarly analysed as those performed by Marec for Keplerian orbits. © 1989.

Aerospace Engineering (ENGI)
: Scopus
Last Update: 2026-06-25
: 2-s2.0-45149145941
PII: 0094576589901057