Satellite cluster distributed control method and device

A distributed control and satellite cluster technology, applied in the aerospace field, can solve the problems of strong dependence on on-board computing power and poor robustness, and achieve the effects of improving autonomous cluster capabilities, improving robustness, and reducing computing load

Pending Publication Date: 2021-07-23
CHINA ACADEMY OF SPACE TECHNOLOGY
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Problems solved by technology

[0004] Based on this, the embodiment of the present invention provides a satellite cluster distributed control method and device to solve the problem of poor robustness of the autonomous cluster control method in the prior art and strong dependence on on-board computing power

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  • Satellite cluster distributed control method and device
  • Satellite cluster distributed control method and device

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Embodiment Construction

[0078] In the following description, specific details such as specific system structures and technologies are presented for the purpose of illustration rather than limitation, so as to thoroughly understand the embodiments of the present invention. It will be apparent, however, to one skilled in the art that the invention may be practiced in other embodiments without these specific details.

[0079] In order to illustrate the technical solutions of the present invention, specific examples are used below to illustrate.

[0080] see figure 1 , which is a schematic diagram of the implementation flow of an embodiment of the satellite cluster distributed control method provided in this embodiment, and is described in detail as follows:

[0081] Step S101, initializing the orbit parameters of the target satellite, the position parameters of each space debris and the position parameters of each satellite in the satellite cluster.

[0082] This embodiment provides a satellite cluste...

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Abstract

The invention relates to the technical field of spaceflight, and provides a satellite cluster distributed control method and device. The method comprises the steps of initializing the orbit parameter of a target satellite, the position parameter of each space debris, and the position parameter of each satellite in a satellite cluster; mapping the satellite cluster into a pigeon group according to the orbit parameter, the position parameter of each space debris and the position parameter of each satellite, and determining a pigeon group interaction mode according to the pigeon group; and calculating pigeon control input according to the pigeon group interaction mode, mapping the pigeon group back to the satellite cluster based on the pigeon control input, and drawing a satellite cluster trajectory. According to the method, the robustness of the large-scale satellite group system in the clustering process is improved, and the calculation load on a single satellite is reduced, so that the autonomous clustering capability of the satellite group system in a complex environment is effectively improved.

Description

technical field [0001] The invention relates to the field of aerospace technology, in particular to a satellite cluster distributed control method and device. Background technique [0002] With the rapid development of the aerospace industry, the number of space missions is increasing and the complexity of missions is increasing. Traditional solutions based on a single large spacecraft often have defects such as high development costs, poor in-orbit flexibility, and limited single-body capabilities. Therefore, The application and development of satellite clusters has become the future trend and strategic focus of today's space development. Satellite cluster system, as a distributed satellite system, can realize information interaction and task collaboration by keeping multiple satellites in a relatively close space area with the help of inter-satellite communication links, and complete complex on-orbit tasks. The rapid changes and the slow response of artificial assistance ...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64G1/10B64G1/24
CPCB64G1/1085B64G1/242
Inventor 邱华鑫周庆瑞王晓初孙昌浩冯宇婷
Owner CHINA ACADEMY OF SPACE TECHNOLOGY
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