Definition of the topological structure of the automatic control system of spacecrafts

Тип публикации: доклад, тезисы доклада, статья из сборника материалов конференций

Конференция: 17th International Scientific Conference on Reshetnev Reading; Krasnoyarsk, RUSSIA; Krasnoyarsk, RUSSIA

Год издания: 2015

Идентификатор DOI: 10.1088/1757-899X/70/1/012013

Ключевые слова: Automation, Control systems, Integer programming, Mathematical programming, Orbits, Rock mechanics, Spacecraft, Structural optimization, Unmanned vehicles, Automated control systems, Directed searches, Geosynchronous orbits, Ground control stations, Orbital periods, Spacecraft control, Spacecraft development, Topological structure, Topology

Аннотация: The paper considers the problem of selection the topological structure of the automated control system of spacecrafts. The integer linear model of mathematical programming designed to define the optimal topological structure for spacecraft control is proposed. To solve the determination problem of topological structure of the control system of spacecrafts developed the procedure of the directed search of some structure variants according to the scheme "Branch and bound". The example of the automated control system of spacecraft development included the combination of ground control stations, managing the spacecraft of three classes with a geosynchronous orbit with constant orbital periods is presented.

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Издание

Журнал: XVII International Scientific Conference Reshetnev Readings

Выпуск журнала: Vol. 70, Is. 1

ISSN журнала: 17578981

Место издания: Bristol

Издатель: IOP Publishing LTD

Авторы

  • Zelenkov P.V. (Siberian State Aerospace University Named after Academician M.F.Reshetnev)
  • Karaseva M.V. (Siberian State Aerospace University Named after Academician M.F.Reshetnev)
  • Tsareva E.A. (Siberian State Aerospace University Named after Academician M.F.Reshetnev)
  • Tsarev R.Y. (Siberian Federal University)

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