A Study of the Motion of Four Linked Satellites Controlled Using Lorentz Forces

Мұқаба

Дәйексөз келтіру

Толық мәтін

Ашық рұқсат Ашық рұқсат
Рұқсат жабық Рұқсат берілді
Рұқсат жабық Рұқсат ақылы немесе тек жазылушылар үшін

Аннотация

This paper considers four satellites connected to each other by electrodynamic tethers, which are assumed to be rigid in the mathematical model of the system’s motion. In the Earth’s magnetic field, current-carrying conductors are affected by Lorentz forces, which are used to control the motion of the system’s center of mass and the angular motion. The paper presents an algorithm for calculating the magnitude of the current to stop the drift of the center of mass of a tetrahedral formation relative to the desired orbital reference frame in low Earth orbit and spin the system up to a constant angular velocity relative to the center of mass. A numerical study of the convergence time to achieve the required motion is carried out depending on the maximum possible current and initial conditions.

Авторлар туралы

K. Chernov

Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, Russia

Email: chernow.kirill@gmail.com
Россия, Москва

D. Ivanov

Keldysh Institute of Applied Mathematics, Russian Academy of Sciences, Moscow, Russia

Хат алмасуға жауапты Автор.
Email: chernow.kirill@gmail.com
Россия, Москва

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© К.С. Чернов, Д.С. Иванов, 2023