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A Method of Tracking and Maintaining an Autonomous Non-cooperative Maneuvering Target on a Satellite

A technology for maneuvering target tracking and maneuvering targets, which is applied in the field of space on-orbit services, can solve problems such as short-range tracking and monitoring, rendezvous and docking, complex capture, tracking spacecraft and losing targets, etc., to achieve simplified calculations, strong engineering applicability, The effect of improving efficiency

Active Publication Date: 2021-02-09
BEIJING INST OF SPACECRAFT SYST ENG
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

Among them, the spacecraft's short-range tracking and monitoring, rendezvous and docking, and capture of non-cooperative targets are extremely complicated
In particular, some non-cooperative targets in space have the ability to maneuver and change orbits. During the process of tracking, surveillance or capture, non-cooperative targets perform maneuvers to change orbits and change their original orbits, thus making the tracking spacecraft lose their targets.

Method used

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  • A Method of Tracking and Maintaining an Autonomous Non-cooperative Maneuvering Target on a Satellite
  • A Method of Tracking and Maintaining an Autonomous Non-cooperative Maneuvering Target on a Satellite
  • A Method of Tracking and Maintaining an Autonomous Non-cooperative Maneuvering Target on a Satellite

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Embodiment Construction

[0033] The present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.

[0034] Such as figure 1 Shown, the present invention a kind of orbit change method that the space non-cooperative maneuvering object is tracked and kept autonomously on the star, and concrete steps are as follows:

[0035] (1) Establish a relative motion model between the tracking spacecraft and the space non-cooperative target spacecraft.

[0036] For the on-board autonomous calculation orbit change method for tracking spacecraft, the relative motion model that needs to be adopted can adapt to the on-board computing resources. Since the tracking spacecraft is tracking and monitoring the non-cooperative space target spacecraft, the relative distance between the two spacecraft is very close, and the perturbation effects are basically the same, so the perturbation is not considered in the relative motion model of the tracking spacecraft and the space n...

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Abstract

The invention provides a method for tracking and maintaining the orbit of an autonomous non-cooperative maneuvering target on a star, using the classic C-W equation as a relative motion model to linearize the relative motion relationship between the tracking spacecraft and the non-cooperative maneuvering target in space On the premise of limited capacity of on-board hardware equipment, on-board autonomous computing can be realized. At the same time, in the design of the track-and-hold orbit change strategy, the ability constraints of the tracking spacecraft are fully considered, and the maximum ignition time constraints of the thrusters of the tracking spacecraft and the minimum time interval constraints between two ignitions are introduced to realize the tracking of the spacecraft under engineering constraints. Design method of space non-cooperative maneuvering target tracking and maintaining orbit change strategy.

Description

technical field [0001] The invention relates to an on-board autonomous non-cooperative maneuvering target tracking, maintaining and orbit changing method, which can be applied to space non-cooperative targets with maneuvering capabilities to perform tracking, maintaining and monitoring tasks, and belongs to the technical field of space on-orbit services. Background technique [0002] With the continuous deepening of human exploration of space, higher requirements are put forward for space technology. Problems such as on-orbit capture and maintenance of spacecraft and space debris removal have become technical problems that need to be faced and solved urgently in the development of aerospace technology. Among them, the spacecraft's short-range tracking and monitoring, rendezvous and docking, and capture of non-cooperative targets are extremely complicated. In particular, some non-cooperative targets in space have the ability to maneuver and change orbits. During the process ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01S19/42
CPCG01S19/428
Inventor 赵峭黄美丽王大轶包泽宇赵小宇李佳宁王永富周静张磊刘德成邹元杰史纪鑫
Owner BEIJING INST OF SPACECRAFT SYST ENG