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Method and system for generating spacecraft collision avoidance strategy

A technology for collision avoidance and spacecraft, applied in the direction of attitude control, etc., can solve problems such as discrepancies, imprecise grouping of orbit control quantities, and spacecraft collision risks, and achieve the effects of prolonging life, saving fuel, and maintaining orbital control safety

Active Publication Date: 2022-05-24
北京航天驭星科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the generation of avoidance strategies, due to the limitation of CPU computing power, the generation speed of avoidance strategies is slow, resulting in imprecise grouping of track control quantities, which is prone to omission. There is a certain deviation in the orbit control, that is, there is a difference between the reality and the theory after the orbit control, resulting in the collision risk of the spacecraft after the orbit control evasion

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  • Method and system for generating spacecraft collision avoidance strategy
  • Method and system for generating spacecraft collision avoidance strategy
  • Method and system for generating spacecraft collision avoidance strategy

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Embodiment Construction

[0047] Embodiments of the invention are described in detail below, but the invention can be practiced in many different ways as defined and covered by the claims.

[0048] As a first embodiment of the present invention, a system for generating a collision avoidance strategy for a spacecraft is provided, such as figure 1 As shown, it includes an input module 1 connected in sequence, a judging and changing track module 2 and a selecting optimal track control quantity module 3 .

[0049] The input module 1 is used to obtain the spacecraft and all space targets that need to be avoided.

[0050] The judging and changing track module 2 includes a first target track forecast module 21 , a first intersection probability calculation module 22 and a first collision risk judgment module 23 . The first target orbit prediction module 21 is used to predict the orbits of the spacecraft and the space target in a first time period in the future. The first rendezvous probability calculation m...

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Abstract

The present invention relates to the technical field of space object collision avoidance, and provides a method and system for generating a spacecraft collision avoidance strategy. The method includes: obtaining the spacecraft and all space objects that need to be avoided; obtaining the first collision warning between the spacecraft and all space objects ; Determine whether the spacecraft has a collision risk, and if so, determine the orbital change time of the spacecraft and the range of orbital control quantities; determine the orbital interval and construct multiple orbital control quantities; obtain spacecraft with different orbital control quantities and all space objects The second collision early warning; determine whether there is a control amount range window length without collision risk greater than or equal to the third specified threshold, if it exists, select the optimal orbit control amount; if it does not exist, adjust the range of the orbit control amount , obtain the second collision warning again until the optimal orbital control amount can be selected. The method and system of the scheme can determine the optimal control strategy to ensure the safety of the spacecraft.

Description

technical field [0001] The present invention relates to the technical field of space target collision avoidance, in particular to a method and system for generating a collision avoidance strategy for a spacecraft. Background technique [0002] With the continuous development of human spaceflight activities, the spatial density of space debris has threatened the safety of spacecraft, especially in low-Earth orbit, the density of debris is even greater, and the number is still increasing rapidly, resulting in spacecraft being hit by space debris Events happen from time to time. The impact of space debris with larger size and mass can change the surface properties of the spacecraft, damage or fail components, and even cause the spacecraft to fail. [0003] Spacecraft collision avoidance refers to an active protection measure taken by spacecraft for catalogued space debris larger than 10 cm. Both NASA and the European Space Agency (ESA) have successfully used orbital maneuver ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05D1/08
Inventor 吴凌根吴新林魏小莹赵磊何镇武张锐王茜吴琳琳
Owner 北京航天驭星科技有限公司