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Spacecraft rendezvous and docking device and method

A technology for rendezvous and docking and spacecraft, applied in the field of spacecraft, can solve the problems of interactive docking failure, reduce docking safety, deviation, etc., and achieve the effect of improving the probability of success and improving safety.

Inactive Publication Date: 2018-07-10
PLA STRATEGIC SUPPORT FORCE INFORMATION ENG UNIV PLA SSF IEU
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  • Summary
  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0007] However, in the above-mentioned stages of interactive docking, such as the final approach stage and the docking and docking stage, the astronauts need to adjust the tracking spacecraft according to the relative position of the tracking spacecraft and the target spacecraft so that it is aligned with the initial aiming point. There may be a certain deviation in this manual alignment method, which will lead to the failure of interactive docking and reduce the safety of docking

Method used

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  • Spacecraft rendezvous and docking device and method
  • Spacecraft rendezvous and docking device and method
  • Spacecraft rendezvous and docking device and method

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Embodiment Construction

[0033] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0034] see figure 1 , which shows a structure of the spacecraft rendezvous and docking device provided by the embodiment of the present invention, which is used to automatically guide and track the spacecraft to accurately align the initial aiming point of the target spacecraft, so as to improve the probability of successful rendezvous and do...

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Abstract

The invention provides a spacecraft rendezvous and docking device and method. Images of at least three light sources in the spacecraft rendezvous and docking device are obtained by an image obtainingdevice in the spacecraft rendezvous and docking device; according to the obtained images, information of the relative position between the image obtaining device and a target spacecraft is obtained, and therefore a tracking spacecraft can be automatically guided to an initial aiming point of the target spacecraft based on the information of the relative position; and manual adjusting links can beomitted at the final approaching stage and parking and docking stage during mutual docking, the tracking spacecraft can be precisely aligned with the initial aiming point of the target spacecraft through an automatic aligning mode, the success possibility of rendezvous and docking is increased, and thus docking safety is improved.

Description

technical field [0001] The invention belongs to the technical field of spacecraft, and more specifically relates to a spacecraft rendezvous and docking device and method. Background technique [0002] With the continuous development of aerospace technology, rendezvous and docking plays a vital role in the docking process of the target spacecraft and the tracking spacecraft. Through rendezvous and docking, the interactive identification between the target spacecraft and the tracking spacecraft and the tracking spaceflight can be realized. positioning of the target spacecraft. At present, the rendezvous and docking includes four stages: ground guidance, short-distance guidance, final approach, and docking and docking. The working process between the target spacecraft and the tracking spacecraft in these four stages is as follows: [0003] In the ground guidance phase, the tracking spacecraft undergoes several orbit-changing maneuvers with the support of ground measurement and...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/64
CPCB64G1/646
Inventor 曲晶于大鹏宋力张涛何中阳朱义君张剑于宏毅
Owner PLA STRATEGIC SUPPORT FORCE INFORMATION ENG UNIV PLA SSF IEU
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