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Missile image guiding system

A guidance system and imaging technology, applied in guidance methods, weapon accessories, offensive equipment, etc., can solve the problems of ineffective stealth technology and decoy bombs, easy to be induced by decoy bombs, easy to be interfered, etc.

Inactive Publication Date: 2013-04-24
叶锋
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] In order to overcome the deficiencies existing in existing missile guidance systems such as difficulty in finding and locking aircraft with stealth technology, easy interference, and easy induction by decoy bombs, the present invention provides a missile image guidance system, which can not only make The stealth technology and decoy bomb technology of the existing aircraft are invalid, and they can resist the interference of electronic interference, infrared interference and other interference means

Method used

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Embodiment Construction

[0012] exist figure 1 Among them, positioning camera (1), transmission gear (2), power gear (3), positioning camera (4), positioning gear (5), image processing chip (6), motor (7), positioning gear (8), Image processing chip (9), processing chip (10), motor (11), motor (12), rudder board (13), rudder board (14), memory chip (15), main tracking camera (16), data import interface (17).

[0013] exist figure 2 In, camera (1), camera (4), support gear (5), support gear (8), attack target (18), gear center point (A), gear center point (B), between attack target and AB Angle (α), angle between attack target and BA (β), distance between missile and attack target (h), distance between AB (s).

[0014] The electronic control system of the image guidance system, the specific implementation technical scheme is as follows: the data import interface (17) is connected with the memory chip (15) through the data line, the memory chip (15) is connected with the processing chip (10) through...

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Abstract

A missile image guiding system is mainly applied to an antiaircraft missile. A missile which has the advantages of resisting jamming ways like electronic jamming and infrared jamming and the like, and deactivating stealth technology and decoy flare technology of existing airplanes and the like can be designed through an electronic control system, a positioning device of an image tracking system, a target search method of the image tracking system, and a multiple image center point tracking method of the image tracking system.

Description

Technical field [0001] The invention relates to a missile image guidance system, which is mainly used in anti-aircraft missiles. Background technique [0002] At present, the guidance systems of known missiles mostly use radar or infrared guidance, but these guidance systems have problems such as being difficult to find and lock aircraft with stealth technology, and being easy to be interfered and induced by decoy bombs. When a country with absolute air superiority conducts asymmetric operations against a country that lacks air control capability, the country that lacks air control capability often lacks effective countermeasures to fight back. Contents of the invention [0003] In order to overcome the deficiencies existing in existing missile guidance systems such as difficulty in finding and locking aircraft with stealth technology, easy interference, and easy induction by decoy bombs, the present invention provides a missile image guidance system, which can not only ma...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F41G3/00
Inventor 叶锋
Owner 叶锋
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