Multi-satellite collaborative ground verification system application mode design method

A verification system and application mode technology, applied in the field of spacecraft testing, can solve problems such as multi-satellite collaborative ground verification systems that have not yet been seen, and achieve the effect of improving authenticity

Pending Publication Date: 2020-11-13
SHANGHAI SATELLITE ENG INST
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Problems solved by technology

There is no systematic description that can support the multi-satellite cooperative ground simulation verification method. At the same time, there is usually a certain gap between the simulation system simulated by the mathematical model and the satellite in-orbit flight environment. The multi-satellite cooperative ground simulation system needs to be able to simulate, test, The test and in-orbit links provide technical support, so the application mode design is equally important, but so far, there is no application mode design method for the multi-satellite collaborative ground verification system

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  • Multi-satellite collaborative ground verification system application mode design method
  • Multi-satellite collaborative ground verification system application mode design method
  • Multi-satellite collaborative ground verification system application mode design method

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Embodiment Construction

[0035] The present invention will be described in detail below in conjunction with specific embodiments. The following examples will help those skilled in the art to further understand the present invention, but do not limit the present invention in any form. It should be noted that those skilled in the art can make several changes and improvements without departing from the concept of the present invention. These all belong to the protection scope of the present invention.

[0036] A multi-satellite collaborative ground verification system application mode design method, comprising the following steps:

[0037] In step 1, the multi-satellite cooperative ground verification system consists of application layer, service layer and resource layer, such as figure 1 shown. Combined with the upper layer of the star, a visual closed-loop verification of the effectiveness of multi-satellite collaboration is realized. The ground test verification system resource layer can set the p...

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Abstract

The invention provides a multi-satellite collaborative ground verification system application mode design method. The method comprises the following steps: 1, constructing a framework of the multi-satellite collaborative ground verification system; 2, carrying out overall design of an application mode according to the architecture of the multi-satellite collaborative ground verification system; 3,designing a ground simulation test mode; 4, designing an on-orbit data drive playback mode; 5, designing an on-orbit data driving parameter adjustment mode. Through simulation system mode regulationand control, full-process development and full-cycle support of a satellite are supported, a satellite-borne task planning prototype system is accessed to a scene simulation system, on-orbit data of the satellite is fully utilized, the model accuracy and the authenticity of a test data set can be improved, and the system calculation and process correctness can be rapidly simulated and evaluated inreal time.

Description

technical field [0001] The invention relates to the technical field of spacecraft testing, in particular to an application mode design method for a multi-satellite cooperative autonomous task planning ground simulation system. Background technique [0002] As people rely more and more on space information support, it is not enough to obtain local or global information through one or two satellites or a certain type of satellite. Multi-satellite network or formation for cooperative detection missions has become As an inevitable trend of development, a series of space multi-satellite distributed earth observation systems have emerged, such as TOPSAT system, Techsat-21 system, A-Train and Morning constellation, F6 system, etc., among which F6 system is a distributed system built by DAPPA. In the satellite system, each satellite is connected wirelessly, and the platform module, data transmission module, and multi-load module are installed on different satellites, and the network...

Claims

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Application Information

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IPC IPC(8): G06F30/20G06Q10/06
CPCG06F30/20G06Q10/0639
Inventor 王壮张海崔本杰赵桥张永贺解加华仲惟超伍国威党建成赵传军
Owner SHANGHAI SATELLITE ENG INST
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