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A launch mission design system and method for emergency applications

A design system and emergency response technology, applied in the direction of design optimization/simulation, special data processing applications, etc., can solve the problem of providing quick view information of disaster situations, but cannot provide support for top-level decision-making of earthquake relief, and does not propose civil emergency application information service launch tasks quickly design methods etc.

Active Publication Date: 2021-11-09
NAT SPACE SCI CENT CAS
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AI Technical Summary

Problems solved by technology

However, the existing satellites often cannot meet the requirements of emergency applications for spatial information in terms of time, spatial resolution, and information types.
Especially in response to the emergency needs of earthquake emergencies in a certain area, there is no complete launch task rapid design method and system for civilian emergency application information services, and it cannot provide disaster quick-view information within three hours. Provide support for top-level decision-making of rescue

Method used

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  • A launch mission design system and method for emergency applications
  • A launch mission design system and method for emergency applications
  • A launch mission design system and method for emergency applications

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Embodiment Construction

[0034] The present invention will be further described in detail below in conjunction with the accompanying drawings.

[0035] like figure 1 As shown, the present invention provides a launch mission design system for emergency applications, the system comprising:

[0036] The launch deployment area module is used to obtain the available resource library; wherein the available resource library includes: the launch point library of the satellite, and the launch point data deployed and carried by each launch point to form an available resource library; wherein, the launch point data Including: the name of the launch point, the position of the launch point, the longitude and latitude of the launch point, the number of carriers at the launch point, the carrying capacity, the type of payload that can be carried, the launch direction information, the available satellite platform and satellite orbit template information; the The satellite orbit template information includes: orbit he...

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Abstract

The present invention provides a launch mission design system for emergency applications, the system includes: a launch deployment area module, used to obtain an available resource library; the available resource library includes: a satellite launch point library, and each launch point deployment Carried launching point data; track design module, used to adopt reverse track design, obtain track design plan, and send it to launch task management module; ballistic design module, used to get ballistic design plan, and return it to launch task Management module; launch task management module, which is used to analyze and obtain emergency response information from emergency response tasks sent by users; summarize and integrate emergency response information, available resource library, orbital design scheme, and ballistic design scheme to form an emergency response The launch mission scheme for the mission.

Description

technical field [0001] The invention relates to the technical field of civil emergency applications, in particular to a launch mission design system and a method for emergency applications. Background technique [0002] With the continuous development of space technology, space information emergency services have gradually shown great application potential in the field of civil emergency applications, and have become an effective means for mankind to fight against various disasters and emergencies. However, due to the diversity and complexity of application types, different civil emergency applications have different requirements for emergency response systems in various aspects and information services. At the same time, the application level of the civil emergency industry has gradually improved, prompting it to put forward higher requirements for space emergency information services: it is urgent to determine the system response time, orbit coverage, revisit cycle indicat...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G06F30/20
CPCG06F30/20
Inventor 谢文明彭晓东杨震时蓬张玉珠刘瑞花
Owner NAT SPACE SCI CENT CAS
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