Missile hang-off life detection method and device, computer equipment and storage medium

A detection method, computer program technology

Inactive Publication Date: 2020-04-28
CHINA ELECTRONICS PROD RELIABILITY & ENVIRONMENTAL TESTING RES INST
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  • Abstract
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  • Claims
  • Application Information

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Problems solved by technology

[0004] Based on this, it is necessary to provide a missile hanging life testing method, device, computer equipment and storage medium for the poor reliability of the traditional missile flying life verification method.

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  • Missile hang-off life detection method and device, computer equipment and storage medium
  • Missile hang-off life detection method and device, computer equipment and storage medium
  • Missile hang-off life detection method and device, computer equipment and storage medium

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Embodiment Construction

[0032] In order to facilitate the understanding of the present application, the present application will be described more fully below with reference to the relevant drawings. Preferred embodiments of the application are shown in the accompanying drawings. However, the present application can be embodied in many different forms and is not limited to the embodiments described herein. On the contrary, the purpose of providing these embodiments is to make the understanding of the disclosure of the application more thorough and comprehensive.

[0033] see figure 1 , a method for detecting the flying life of a missile, comprising step S200, step S300 and step S400.

[0034] In step S200, a comprehensive environmental curve is obtained according to the combat mission profile of the missile carried by the helicopter and the corresponding environmental parameters.

[0035] Specifically, the flight life refers to the total flight times or total flight time of helicopter-borne missil...

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Abstract

The invention relates to a missile hang-off life detection method and device, computer equipment and a storage medium. The method comprises the following steps: firstly, according to a combat missionprofile of a helicopter-borne missile in an actual combat environment and corresponding environmental parameters, establishing a comprehensive environment curve, establishing a test profile accordingto the comprehensive environment curve and a combat mission profile to simulate the actual use environment of the helicopter-borne missile, and finally carrying out a simulation hang-flight test on the helicopter-borne missile according to actually required preset parameter indexes, thereby detecting whether the hang-flight life of the helicopter-borne missile meets requirements or not. Through the above scheme, whether the hang-off life of the helicopter-borne missile meets the requirements can be known without carrying out a range test on the helicopter-borne missile, and life assessment ofthe helicopter-borne missile is achieved; compared with a traditional verification method, the method has the advantages that missile resource waste will not be caused, the implementation difficulty is low, the cost is low, the period is short, the fault problem of the helicopter-borne missile can be exposed in time, and the verification reliability is high.

Description

technical field [0001] The present application relates to the technical field of life detection, in particular to a method, device, computer equipment and storage medium for life detection of a missile in flight. Background technique [0002] With the continuous development of military technology, there are more and more types of national defense weapons. Among them, helicopter-borne missiles can be mounted on helicopters to operate, thereby realizing long-distance combat. When the missile is mounted on a helicopter and flies at high altitude and high speed, it will be pulled by various extreme temperatures and large overloads, and it is easy for the missile to reach its flight life. Therefore, in actual work, knowing the flying life of the missile is of great significance for the helicopter to carry the missile to complete the combat mission. [0003] Helicopter-borne missiles will be verified for flight life indicators before use. The traditional method of missile flight ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F30/20G06F119/14
Inventor 许胜刚李劲陆家乐蔡自刚杨司邦蔡汝山
Owner CHINA ELECTRONICS PROD RELIABILITY & ENVIRONMENTAL TESTING RES INST
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