Timing air injection tethered combination dragging deorbiting method and system based on winding and unwinding device

Abstract

The invention discloses a timing air injection tethered combination dragging deorbiting method and system based on a winding and unwinding device. The timing air injection tethered combination dragging deorbiting method and system can be applied to a dragging removal task after a space flying net captures a target. For a space control unstable target, after the flying net is used for capturing thetarget, a task satellite pulls a tether once at set intervals to generate tension in a fixed-time air injection mode, so that the target is dragged to deorbit. In a non-air-injection time period, therelative distance between two satellites is close, and the tether may loosen; a threshold value is designed for the loosening degree of the tether; when the loosening degree of the tether exceeds thethreshold value, a tether winding and unwinding device is adopted for winding the tether, and it is guaranteed that the loosening length of the tether is within a certain range; when the relative distance between the two satellites is smaller than the threshold value after multiple times of tether winding, the task satellite jets and moves away, and meanwhile, constant small tension is generatedthrough the constant tension generating capacity of the winding and unwinding device.

Description

technical field [0001] The invention relates to a method and system for dragging and derailing an air jet rope assembly based on a retractable device, and belongs to the technical field of dragging and derailing control of a rope assembly. Background technique [0002] GEO orbit has wide application value because of its particularity relative to the ground. It is a very important scarce resource and plays a pivotal role in the space strategy of various space countries. With the increasing demand of various countries for communication, broadcasting, meteorology, navigation and other fields, more and more aircrafts entering this limited space are becoming more and more crowded, and the demand for GEO orbital garbage removal is particularly urgent. [0003] The existence of space debris seriously threatens the safety of orbiting spacecraft. The collision between them and the spacecraft will change the performance of the spacecraft, cause damage to the surface components, cause ...

AI Technical Summary

Problems solved by technology

[0003] The existence of space debris seriously threatens the safety of orbiting spacecraft. The collision between them and the spacecraft will change the performance of the spacecraft, cause damage to the surface components, cause failure of the spacecraft system, and affect the life of the spacecraft.

[0004] At present, the space capture mainly uses the robotic arm, and although the mechanical arm capture is fine in operation, it has high requirements for orbit control and attitude control accuracy, high precision requirements for measuring equipment, short operating distance, high risk, and selective capture. Disadvantages such as location

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