A simulation device for manipulating the configuration of micro-satellites using the interaction force of high-temperature superconducting permanent magnets

Abstract

The invention provides a simulation device for manipulating the micro-satellite configuration by using the interaction force of high-temperature superconducting permanent magnets, which relates to the technical field of micro-satellite configuration adjustment, which includes a permanent magnet carrier and a superconducting carrier suspended side by side, and a permanent magnet The stage is fixedly connected with a rotating shaft permanent magnet, and fixed on both sides of the rotating shaft permanent magnet is a variable field magnetic conducting rod that changes the magnetic field of the rotating shaft permanent magnet. The superconducting stage is rotatably connected with a rotating shaft superconductor placed in the first liquid nitrogen box. ; The superconducting stage is provided with a rotating shaft and a limit device, so that the superconducting stage can rotate at a certain angle relative to the superconductor of the rotating shaft; the permanent magnet stage and the superconducting stage are provided with an initial stage that interacts through the magnetic flux pinning effect. The positioning component and the last position positioning component; the permanent magnet carrier and the superconducting carrier are independently provided with a first flywheel component and a second flywheel component. The invention solves the problem in the prior art that adjusting the micro-satellite configuration can only be realized by consuming the fuel carried by the star itself, which leads to the short life of the star on orbit.

Description

technical field [0001] The invention relates to the technical field of micro-satellite configuration adjustment, in particular to a simulation device for manipulating the configuration of micro-satellites by utilizing the interaction force of high-temperature superconducting permanent magnets. Background technique [0002] Micro-satellite cluster flight has broad application prospects in synthetic aperture telescopes and space communications. This application also requires that satellite clusters have the ability to independently maintain their mutual spatial positions, and at the same time have the ability to adjust the combined configuration of micro-satellite clusters. The traditional method of adjusting a satellite's configuration is by consuming fuel carried by the star itself. Due to the limited ability of the star to carry fuel, in order to prolong the on-orbit life of the star as much as possible, it is necessary to find a new configuration maintenance and configura...

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Problems solved by technology

[0004] Aiming at the above-mentioned problems in the prior art, the present invention provides a simulation device for controlling the micro-satellite configuration by using the interaction force of high-temperature superconducting permanent magnets, which solves the problem that in the prior art, the adjustment of the micro-satellite configuration can only be done by consuming the star itself. The fuel carried to achieve the problem that leads to the short life of the star in orbit

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