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(Reference retrieved automatically from Web of Science through information on FAPESP grant and its corresponding number as mentioned in the publication by the authors.)

Errors of Powered Swing-By in the Restricted Three-Body Problem

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Author(s):
Ferreira, Alessandra F. S. [1, 2] ; Moraes, V, Rodolpho ; Prado, Antonio F. B. A. [3] ; Winter, Othon C. [4, 5]
Total Authors: 4
Affiliation:
[1] Paulista State Univ UNESP, BR-12516410 Guaratingueta - Brazil
[2] Dept Math, Sao Paulo - Brazil
[3] Natl Inst Space Res INPE, BR-12227010 Sao Jose Dos Campos - Brazil
[4] Moraes, Rodolpho, V, Paulista State Univ UNESP, BR-12516410 Guaratingueta - Brazil
[5] Moraes, Rodolpho, V, Dept Math, Sao Paulo - Brazil
Total Affiliations: 5
Document type: Journal article
Source: JOURNAL OF GUIDANCE CONTROL AND DYNAMICS; v. 42, n. 10, p. 2246-2257, OCT 2019.
Web of Science Citations: 0
Abstract

The powered swing-by maneuver is described by the parameters that define the orbit of the spacecraft and the ones that define the impulse applied. In this case the impulse is applied in the periapsis of the orbit around the body used for the close approach. It is important to consider that the values of the parameters involved in this maneuver are susceptible to errors, in particular the ones relative to the impulse, which can affect the energy variation and, consequently, the orbit obtained after the maneuver. This paper has the goal of studying several aspects related to the optimization of this maneuver, particularly verifying the sensitivity of the maneuver to these parameters and the effects that their errors make in a swing-by maneuver. The errors coming from the impulsive maneuver is the most important problem when considering powered swing-by, and it is usually the main reason to avoid this technique. Therefore, this paper will study the effects of these errors and compare them with the errors due to other variables involved in the close approach. It also shows the best direction to apply the impulse, as a function of the impulse magnitude and the regions of optimality of this maneuver. (AU)

FAPESP's process: 16/23542-1 - Swing-By maneuvers with use of Impulses and Cables in Three Dimensions
Grantee:Alessandra Ferraz da Silva Ferreira
Support type: Scholarships in Brazil - Post-Doctorate
FAPESP's process: 16/24561-0 - On the relevance of small bodies in orbital dynamics
Grantee:Othon Cabo Winter
Support type: Research Projects - Thematic Grants
FAPESP's process: 16/14665-2 - Astrodynamics applied to space vehicles.
Grantee:Antônio Fernando Bertachini de Almeida Prado
Support type: Regular Research Grants