Space debris rope system dragging despinning and removal method

A technology for space debris and cleaning methods, applied in the directions of transportation and packaging, aerospace equipment, tools, etc., can solve the problems of falling off protruding parts, broken tethers, low redundancy, etc., and achieve the effect of reducing the risk of debris loss of control

Active Publication Date: 2016-11-16
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, there are obvious disadvantages in the prior art: generally speaking, space debris is in a rotating state, and the protruding parts on the debris (such as solar panels, etc.) may be entangled and cut with the tether, causing the protruding parts to fall off or the tether to break, thereby Cause the cleanup task to fail, and even cause more debris to be generated
The single-rope tethered trailer system has the problem of low redundancy

Method used

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  • Space debris rope system dragging despinning and removal method
  • Space debris rope system dragging despinning and removal method
  • Space debris rope system dragging despinning and removal method

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Embodiment 1

[0059] In order to verify the feasibility of the method, a set of numerical simulation results are given below. The numerical simulation parameters such as geometric and physical parameters of the rope trailer system are listed in Table 1.

[0060] Table 1 Numerical simulation parameters

[0061]

[0062]

[0063] A space debris tether drag derotation and cleaning method disclosed in this embodiment can be implemented according to the following steps, see figure 2 .

[0064] Step 1: Launch the trailer spacecraft into orbit and complete the rendezvous with the debris.

[0065] Step 2: Attach the trailer to the debris with the help of two tethers.

[0066] Step 3: Establish the dynamic model of the double-tether trailer system, design the control law to adjust the nominal rope length of the two tethers, so as to change the tension of the tethers, and derotate the debris under the cooperation of the two ropes to avoid the protruding parts on the debris. The tether crea...

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Abstract

The invention discloses a space debris rope system dragging despinning and removal method, relates to space debris despinning and removal methods and belongs to the technical field of spaceflight. By the adoption of the method, a trailer spacecraft is launched into an orbit, so that the rendezvous with debris is finished; a trailer is connected with the debris through multiple tying ropes; a dynamical model is established, a control law is designed to adjust the nominal rope length of each tying rope to change the tension of the tying ropes, despinning of the debris is achieved through the cooperation of the multiple tying ropes, the situation that the tying ropes are cut and broken through protruding components on the debris is avoided, and the stability and the redundancy of a rope system trailer system are improved; and a trailer engine is used for ignition, reverse dragging force is applied, the space debris is pulled into the atmosphere to be burnt, and therefore debris removal is achieved. By the adoption of the method, despinning of the space debris can be achieved, the situation that the tying ropes are cut and broken through the protruding components on the debris is avoided, and the stability of the system is improved; and in addition, the redundancy of the tying ropes is improved by increasing the number of the tying ropes. The method can be used for space debris despinning and removal and can also be used for despinning of and control over other non-cooperative targets.

Description

technical field [0001] The invention relates to a space debris derotation and cleaning method, in particular to a space debris derotation and cleaning method using a tether dragging method, which belongs to the field of aerospace technology and can be used for space debris (abandoned satellites, upper stages of rockets, explosions, etc.) It can also be used for racemization and control of other non-cooperative targets. Background technique [0002] Since the former Soviet Union successfully launched the first man-made earth satellite in 1957, the amount of space debris has experienced rapid and continuous growth along with human spaceflight activities. According to the latest report data released by the NASA Orbital Debris Project Office, as of April 6, 2016, 17,385 large-scale orbiting targets have been monitored, including 4,041 payloads and 13,344 rocket bodies, and debris larger than 1 cm in diameter The total number is estimated to be on the order of millions, and they...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G4/00
CPCB64G4/00
Inventor 祁瑞张景瑞
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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