Optimal low-thrust transfers between close near-circular coplanar orbits

Autor:	Anatoly A. Baranov, V. Yu . Razumny, A. F. B. de A. Prado, A. A. Baranov
Rok vydání:	2011
Předmět:	Physics Mathematical analysis Coordinate system Process (computing) Aerospace Engineering Astronomy and Astrophysics Thrust Propulsion Space and Planetary Science Transfer (computing) Transversal (combinatorics) Orientation (geometry) Orbit (dynamics) Astrophysics::Earth and Planetary Astrophysics
Zdroj:	Cosmic Research. 49:269-279
ISSN:	1608-3075 0010-9525
DOI:	10.1134/s0010952511030014
Popis:	Four types of optimal solutions are demonstrated to exist for transfers (time of flight is not fixed) between close near-circular coplanar orbits. One solution is realized with the help of fixed orientation of the propulsion system (PS) along a transversal in the orbital coordinate system. Another is reached at fixed orientation of the PS in the inertial coordinate system. The third and fourth types of solutions change the PS orientation in the process of executing the maneuver. Regions of existence are established for all types of solutions, and algorithms for determination of parameters of these maneuvers are suggested. The algorithms were used to calculate parameters of the maneuvers of transfer from a launching orbit to a working Sun-synchronous orbit, and to calculate the maneuvers of supporting the parameters of such an orbit in a specified range.
Databáze:	OpenAIRE
Externí odkaz:	https://explore.openaire.eu/search/publication?articleId=doi_________::aec4e05032b2f83ee247fcfadcffbeb4 https://doi.org/10.1134/s0010952511030014 Zobrazit plný text záznamu Plný text ve formátu PDF