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Gyroplane guided missile attack system

A technology for rotorcraft and missiles, which can be used in self-propelled missiles, offensive equipment, projectiles, etc., and can solve problems with high financial and technical requirements

Inactive Publication Date: 2020-11-20
航天科工通信技术研究院有限责任公司
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  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] At present, the air-guided missile attack system mainly uses helicopters, bombers and fighter jets to achieve the attack tasks on ground stationary targets, ground moving targets, and low-altitude moving targets, which requires high funds and technology.
When the autogyro performs an attack mission, it needs to actively obtain the attributes, positions, and states of the target. It needs to combine the flight attitude of the autogyro and use the fire control computer to calculate and control the aiming of intelligent missiles. Only by launching under the control of the program can an effective attack on the target be achieved. Therefore, the guided missile attack system of the autogyro has not yet been used.

Method used

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  • Gyroplane guided missile attack system

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Embodiment Construction

[0024] The core of the present invention is to provide a self-rotating rotor mechanism guided missile attack system, which can realize low-cost, long-distance, high-precision and flexible launch attack missions without using helicopters, bombers and fighter jets.

[0025] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments It is a part of embodiments of the present invention, but not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.

[0026] refer to figure 1 , a kind of autorotor mechanism guided missile attac...

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Abstract

The invention discloses a gyroplane guided missile attack system. The gyroplane guided missile attack system comprises a gyroplane, a fire control computer, a weapon hanging frame, a guided missile, adata link, a reconnaissance pod, an attitude and heading instrument and a power distribution box. According to the gyroplane guided missile attack system, the gyroplane platform is utilized, and thefire control computer, the weapon hanging frame, the guided missile, the data link, the reconnaissance pod, the attitude and heading instrument and the power distribution box are hung, so that the determination, aiming and attack efficiency of a ground static target, a ground moving target and a low-altitude moving target is achieved. The gyroplane guided missile attack system is suitable for mounting guided missiles for autonomous guidance, homing guidance, remote control guidance, composite guidance and the like. The gyroplane guided missile attack system achieve pilot launching, remote command and control center launching and program launching, and the launching attack task of a guided missile is completed. The gyroplane guided missile attack system has the advantages of being low in cost, long in distance, high in precision and flexible in launching.

Description

technical field [0001] The invention relates to the technical field of autorotor aircraft and guided missiles, in particular to an autorotor aircraft guided missile attack system. Background technique [0002] The autogyro is mainly used for extreme sports, and the air patrol mission is gradually being carried out, and the mission of using the autogyro to realize the guided missile attack has not yet been carried out. [0003] At present, the air-guided missile attack system mainly uses helicopters, bombers and fighter jets to achieve the attack tasks on ground stationary targets, ground moving targets, and low-altitude moving targets, which requires high funds and technology. When the autogyro performs an attack mission, it needs to actively obtain the attributes, positions, and states of the target. It needs to combine the flight attitude of the autogyro and use the fire control computer to calculate and control the aiming of intelligent missiles. Only by launching unde...

Claims

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Application Information

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IPC IPC(8): F42B15/00F42B15/01F42B10/26
CPCF42B15/00F42B15/01F42B10/26
Inventor 熊维族
Owner 航天科工通信技术研究院有限责任公司
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