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Method and system for configuring multi-satellite collaborative resources

A configuration method and resource technology, applied in the aerospace field, can solve the problem of low utilization rate of satellite resources, and achieve the effect of improving the utilization rate of satellite resources and efficient configuration

Active Publication Date: 2022-05-24
HEFEI UNIV OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0006] Aiming at the deficiencies of the prior art, the present invention provides a method and system for configuring multi-satellite cooperative resources, which solves the technical problem of low utilization rate of satellite resources in the prior art

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  • Method and system for configuring multi-satellite collaborative resources
  • Method and system for configuring multi-satellite collaborative resources
  • Method and system for configuring multi-satellite collaborative resources

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Embodiment Construction

[0094] In order to make the purposes, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention are described clearly and completely. Obviously, the described embodiments are part of the embodiments of the present invention, rather than all the implementations. example. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0095] The embodiments of the present application solve the technical problem of low utilization rate of satellite resources in the prior art by providing a method and system for configuring multi-satellite cooperative resources, and improve the utilization rate of satellite resources.

[0096] The technical solutions of the embodiments of the present application are to solve the above-mentioned technical p...

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Abstract

The invention provides a method and system for configuring multi-satellite collaborative resources, which relate to the field of aerospace. The method includes the following steps: obtaining satellite resources; selecting satellite resources based on the task requirements of the tasks to be performed, and obtaining resource clusters corresponding to the tasks to be performed; vectorizing the satellite capabilities of the satellite resources; vectorizing the task requirements of the tasks to be performed; Obtain the resource cluster capability of the satellite capability; obtain the income of each task to be executed; obtain the objective function based on the income of all tasks to be executed; obtain the demand energy constraint based on the vectorized task requirements and resource cluster capabilities; based on all satellite resources and resources Cluster acquisition resource energy constraints; vectorized satellite capability and resource cluster capability acquisition capability energy constraints; construct a dynamic resource alliance model based on objective function, demand energy constraints, resource energy constraints, and capability energy constraints; obtain resource alliances based on dynamic resource alliance models . The invention improves the utilization rate of satellite resources.

Description

technical field [0001] The invention relates to the technical field of aerospace, in particular to a method and system for configuring multi-satellite cooperative resources. Background technique [0002] With the development of aerospace technology, Earth observation satellites have attracted more and more attention. Earth observation satellites obtain relevant information by probing the Earth's surface and lower atmosphere. Earth observation satellites have unique advantages such as wide coverage, long duration, and freedom from airspace and national boundaries. Therefore, earth observation satellites are widely used in military reconnaissance, meteorological observation, and environmental protection. [0003] For some complex observation tasks, relying on a single satellite to observe the mission target can often only obtain part of the effective information of the mission target, and cannot efficiently complete the mission requirements. Therefore, in the prior art, mult...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G05B13/04
CPCG05B13/042
Inventor 靳鹏张凯胡笑旋夏维罗贺马华伟王国强任送莲
Owner HEFEI UNIV OF TECH