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Controller design method of cluster satellite system and control method

A satellite system and design method technology, applied in the field of satellite control, can solve the problems of control cost loss, difficulty in precise control, use of directional communication network, etc., to improve time conservatism, solve structure and parameters, and solve design problems difficult effect

Pending Publication Date: 2019-09-06
RES & DEV INST OF NORTHWESTERN POLYTECHNICAL UNIV IN SHENZHEN +1
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Problems solved by technology

[0003] However, there are often some insurmountable problems in the work on finite-time consensus control techniques for multi-agent systems
First of all, the existing finite-time consistency control technology is difficult to achieve precise control in terms of time control, and can only obtain an upper bound of the formation completion time, and this upper bound of time is often very conservative, far greater than the real formation formation time, As a result, there is a huge loss in control costs, which seriously affects the control efficiency
Secondly, the existing finite-time consistent control technology often uses discontinuous technology to design control strategies, which often brings problems such as controller instability in practical applications.
Thirdly, the existing finite-time consistency control technology is often carried out on undirected communication networks, and the actual communication network is more of a directed communication network, which makes it difficult for the existing finite-time consistency control technology to be used in directed communication networks. use on
Finally, the existing finite-time consistency control technology is only suitable for low-order dynamical systems, and it is difficult to apply to general high-order systems

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  • Controller design method of cluster satellite system and control method
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Embodiment Construction

[0011] The technical solutions in the embodiments of the present invention will be clearly and completely described below. Obviously, the described embodiments are only some of the embodiments of the present invention, but not all of them. 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.

[0012] The invention provides a method for designing a controller of a clustered satellite system. The method mainly includes the following steps: first, using formation error analysis technology to carry out formation modeling for the clustered satellite system described by the Hill equation, and transforming the formation problem of the clustered satellite system into Consistency problem of linear high-order multi-agent system; secondly, design a step-by-step control strategy for linear high-order multi-agent system using the speci...

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Abstract

The invention discloses a controller design method of a cluster satellite system and a control method, and relates to the technical field of satellite control, being applicable to formation control ofthe cluster satellite system, and also being further popularized and applied to the design of specified time tracking controller and inclusion controller of the cluster intelligence system; the problem of time conservation of the cluster intelligence system in a coordinated formation problem within limited time is effectively improved, the topological structure of the communication network is greatly expanded, and the design difficulty of the structure and parameter of the specified time consistency formation controller of the cluster satellite system is solved.

Description

technical field [0001] The invention relates to the technical field of satellite control, in particular to a controller design method and a control method for a cluster satellite system. Background technique [0002] The distributed formation of cluster satellite system is an important development trend of deep space exploration in the future, and has broad development prospects. With the rapid development of my country's deep space exploration field, the accuracy requirements of deep space exploration continue to increase, which requires the deep space satellite astronomical telescope to continuously increase its caliber and scale. In recent years, in order to improve the accuracy of deep space exploration and at the same time reduce the difficulty of launching satellite telescopes for deep space exploration, people have proposed the concept of cluster satellite astronomical telescopes for high and deep space exploration. By carrying astronomical telescopes on multiple smal...

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 赵宇刘永芳
Owner RES & DEV INST OF NORTHWESTERN POLYTECHNICAL UNIV IN SHENZHEN
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