@Article{SmirnovMashOvchPrad:2018:TeFoNa,
author = "Smirnov, G. V. and Mashtakov, Y. and Ovchinnikov, M. and Prado,
Antonio Fernando Bertachini de Almeida",
affiliation = "{} and {} and {} and {Instituto Nacional de Pesquisas Espaciais
(INPE)}",
title = "Tetrahedron formation of nanosatellites with single-input
control",
journal = "Astrophysics and Space Science",
year = "2018",
volume = "363",
number = "9",
pages = "e180",
month = "Sept.",
keywords = "Formation flying, Single-input control, Tetrahedral formation.",
abstract = "The present paper studies the formation flight of four
nanosatellites forming a tetrahedron. The main goal of this
research is to find the relative orbits of these satellites that,
at least in the linear Hill-Clohessy-Wiltshire model, ensure
finite relative motion and keep the volume and shape of the
tetrahedron configuration. Since real motions of these satellites
will differ from the linear ones, especially under the influence
of the perturbation, active control is necessary. In addition, the
limited size of the satellites does not allow us to use a complex
3-axis attitude control system. In the present paper we consider
the passive magnetic attitude control system and suppose that the
thrust direction is always aligned with the local geomagnetic
field. In order to increase mission lifetime the control algorithm
that minimizes the propellant consumption and keeps the
tetrahedron volume and shape is investigated.",
doi = "10.1007/s10509-018-3400-4",
url = "http://dx.doi.org/10.1007/s10509-018-3400-4",
issn = "0004-640X",
language = "en",
urlaccessdate = "03 maio 2024"
}