Control de formaciones en vuelo de satélites de bajo coste

  1. Manuel Angulo Jerez 1
  2. Segundo Esteban San Román 1
  3. José María Girón Sierra 1
  4. Óscar Rodríguez Polo 2
  1. 1 Universidad Complutense de Madrid
    info

    Universidad Complutense de Madrid

    Madrid, España

    ROR 02p0gd045

  2. 2 Universidad de Alcalá
    info

    Universidad de Alcalá

    Alcalá de Henares, España

    ROR https://ror.org/04pmn0e78

Book:
XXXIX Jornadas de Automática: actas. Badajoz, 5-7 de septiembre de 2018
  1. Inés Tejado Balsera (coord.)
  2. Emiliano Pérez Hernández (coord.)
  3. Antonio José Calderón Godoy (coord.)
  4. Isaías González Pérez (coord.)
  5. Pilar Merchán García (coord.)
  6. Jesús Lozano Rogado (coord.)
  7. Santiago Salamanca Miño (coord.)
  8. Blas M. Vinagre Jara (coord.)

Publisher: Universidad de Extremadura

ISBN: 978-84-9749-756-5,  978-84-09-04460-3

Year of publication: 2018

Pages: 590-597

Congress: Jornadas de Automática (39. 2018. Badajoz)

Type: Conference paper

DOI: 10.17979/SPUDC.9788497497565.0591 DIALNET GOOGLE SCHOLAR lock_openRUC editor

Abstract

Low-cost satellites are a revolution in the space sector, because they allow you to take risks. Satellite flying formations are risky missions, they are very demanding from the point of view of the control algorithm and the cost of propulsion. These satellites have the handicap of their limited propulsion capacity, and the reduced performance of both sensors and hardware. To ensure that the mission offers sufficient autonomy, it is necessary to study modes of operation that suppose a minimum cost of propulsion. This article presents a mathematical analysis of the problem and proposes different modes of operation that minimize the consumption of the propulsion system, also analyzing different control strategies.

Data source: Dialnet