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Safely and credibly launching control method for missile

A launch control and missile launch technology, applied in program control, computer control, general control system, etc., can solve problems such as lack of launch and attack targets

Active Publication Date: 2013-12-04
TIANJIN JINHANG COMP TECH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In view of the lack of these critical data the missile is just a "naked bomb" and does not have the ability to launch and attack the target

Method used

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  • Safely and credibly launching control method for missile
  • Safely and credibly launching control method for missile
  • Safely and credibly launching control method for missile

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Embodiment Construction

[0035] In order to make the purpose, content, and advantages of the present invention clearer, the specific embodiments of the present invention will be further described in detail below with reference to the accompanying drawings and embodiments.

[0036] In order to solve the problem of the prior art, the technical scheme of the present invention is:

[0037] (1) The overall technical scheme of missile launch control. like figure 2 As shown, the architectural design of the missile launch control computer is modified and a safety control module 202 is added. The security control module is also an embedded computer system in architecture, which mainly realizes the following functions:

[0038] a. Take over the memory and external interface in the launch control computer 101 on the bomb;

[0039] b. Relay control of the reset signal of the embedded processor in the launch control computer 101 on the missile;

[0040] c. Encrypt and save the launch preparation software in t...

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Abstract

The invention belongs to the technical field of missile weaponry launching control, and particularly relates to a safely and credibly launching control method for a missile. The safely and credibly launching control method for the missile particularly relates to a starting operation control method achieved for missile launching preparation software based on safety control methods of identity authentication, real-time authorization and the like. A launching control computer is revised, a safety control module is designed and added, and a set of brand new authentication, identification and starting control process is designed through an external interface, so that reliable and effective missile launching control is achieved. Above all, the strict safety control process for starting and software operation of an embedded type system is designed, so that launching of the missile can be safely and effectively controlled. A severe result possibly caused by misoperations or deliberate sabotage is avoided while reliably launching of the core missile system is ensured, and therefore safety and reliability of the core missile system are ensured.

Description

technical field [0001] The invention belongs to the technical field of missile weapon equipment launch control, in particular to a missile safe and credible launch control method. Background technique [0002] Missiles are the most important weapons and equipment in modern warfare. For the missile system that has been deployed to the position, the launch of the missile is completely carried out by the front-line officers and soldiers of the position. Although for many tactical missiles, strict launch control is not required, front-line officers and soldiers can independently decide and launch according to battlefield conditions. However, for some important core missiles, such as strategic missile systems, safe and effective missile launch control has become a very important matter. On the one hand, such a missile system must ensure that the missile can be reliably launched after the launch order is issued, and on the other hand It is also necessary to ensure that missiles ...

Claims

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Application Information

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IPC IPC(8): G06F21/31G05B19/042
Inventor 王可周津张永华李岩杨阳
Owner TIANJIN JINHANG COMP TECH RES INST
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