图书馆订阅: Guest
自动化与信息科学期刊

每年出版 12 

ISSN 打印: 1064-2315

ISSN 在线: 2163-9337

SJR: 0.173 SNIP: 0.588 CiteScore™:: 2

Indexed in

Use of Equinoctial Orbital Elements as Variables in the Problem of Minimal Time Orbit-to-Orbit Transfer in Strong Gravitational Field under Fixed-Value Thrust

卷 35, 册 8, 2003, 13 pages
DOI: 10.1615/JAutomatInfScien.v35.i8.30
Get accessGet access

摘要

A problem of minimal time transfer between elliptic orbits of a spacecraft (SC) with a small constant magnitude and regulated direction thrust in a central gravitational field is considered. Unlike earlier papers [1, 2], for obtaining averaged equations of optimal motion, in this work the authors used a system of equinoctial orbital elements. This technique enables one to eliminate singularities associated with zero values of either eccentricity or inclination of elliptic orbit in equations of motion.

对本文的引用
  1. Kiforenko Boris M., Vasil’ev Igor Yu., Quasioptimal interorbit transfers of a low-thrust spacecraft in strong central Newtonian gravity field, Acta Astronautica, 65, 1-2, 2009. Crossref

  2. Kiforenko Boris N., Vasil'ev Igor Yu., Tkachenko Yaroslav V., On the problem of optimal control of the thrust value of the electric propulsion rocket with solar energy source, Acta Astronautica, 89, 2013. Crossref

Begell Digital Portal Begell 数字图书馆 电子图书 期刊 参考文献及会议录 研究收集 订购及政策 Begell House 联系我们 Language English 中文 Русский Português German French Spain