4.1 Article

Method of Forming a Triangular Rotating Tethered Constellation of Spacecraft Using Electromagnetic Forces

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Publisher

PLEIADES PUBLISHING INC
DOI: 10.1134/S1064230722040141

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Funding

  1. Russian Science Foundation [21-51-53002]

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This paper investigates the deployment of a tethered constellation and proposes a combined control method for stabilization and control using electromagnetic forces and control mechanisms.
The problem of deploying a tethered constellation of four spacecraft (SC) is considered. The SC from which three tethers with the end small SC (satellites) are released is in the center of the constellation. Once formed, the constellation is a symmetric ray star symmetric SC structure (hub-spoke), stabilized by rotation at some given angular velocity. A combined control method is proposed and analyzed in the formation of a tethered constellation, which consists of the joint use of electromagnetic forces acting on current-conducting tethers in the Earth's magnetic field to create a torque relative to the center of mass of the system and control mechanisms for the release of tethers located in the central SC. The results of numerical calculations are presented, illustrating the application of the considered control laws.

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