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Air-to-ground guided weapon lateral attack method and device

An air-to-ground and weapon technology, which is applied in the direction of guidance, weapon accessories, instruments, etc., can solve the problems of not being able to realize the weapon's side attack ability well, and achieve the effect of easy implementation and transplantation, and simple calculation principle

Active Publication Date: 2019-05-10
北京航天飞腾装备技术有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The present invention provides a method and device for lateral attack of an air-to-ground guided weapon to at least solve the technical problem in the related art that the lateral attack capability of the weapon cannot be well realized due to the limitation of the missile body

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  • Air-to-ground guided weapon lateral attack method and device
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  • Air-to-ground guided weapon lateral attack method and device

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Embodiment Construction

[0026] In order to enable those skilled in the art to better understand the solutions of the present invention, embodiments of the present invention will be described below in conjunction with the accompanying drawings.

[0027] According to an embodiment of the present invention, an embodiment of a method for lateral attack of an air-to-ground guided weapon is provided. It should be noted that although the logical order is shown in the flow chart, in some cases, it may be different from The sequence herein performs the steps shown or described in sequence.

[0028] figure 1 is a flow chart of the air-to-ground guided weapon lateral attack method according to an embodiment of the present invention, such as figure 1 As shown, the method includes the following steps:

[0029] Step S101, obtain the attack target position, predetermined lateral restraint angle ψ c and the real-time flight status of the aircraft, wherein the flight status includes the position, speed, and wind f...

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Abstract

The invention discloses an air-to-ground guided weapon lateral attack method and device, wherein the method comprises the following steps of acquiring an attack target position, a preset lateral constraint angle psi c and a real-time flight state of an aircraft, wherein the flight state comprises a position, a speed and a wind field condition of the aircraft; according to the flight state and thepsi c, determining a virtual target position in a manner of trajectory simulation iterative calculation; then furthermore, determining a flight trajectory of the guided weapon according to the virtualtarget position, the attack target position and the flight state; and according to the flight trajectory, after the guided weapon flies to the virtual target position after being launched, starting aturning program, and then performing lateral attack on an attack target according to the psi c. the air-to-ground guided weapon lateral attack method and device solves the technical problem that thelateral attack capability of the weapon cannot be well achieved due to limitation of a projectile body in the prior art.

Description

technical field [0001] The invention belongs to the field of guidance and control, and relates to a method and a device for lateral attack of an air-to-ground guided weapon. Background technique [0002] In modern warfare, air-to-ground guided weapons can attack targets in many ways, and lateral attack is one of the important attack methods. In related technologies, the lateral attack of the weapon is mostly realized by using the optimal guidance rate, but due to the limitation of the overload of the projectile itself, this method cannot maximize the lateral attack capability of the weapon, and this method can only ensure that when the projectile meets the target Due to the angle constraints, the angle of view before encountering, the remaining flight distance and other indicators cannot be adjusted and controlled, which brings difficulties to the use of air-to-ground guided weapons equipped with seekers. [0003] For the above problems, no effective solution has been propo...

Claims

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Application Information

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IPC IPC(8): F41G3/22G06F17/50
Inventor 王晓燕张超苏泽亚李广王明光张传海周楠吴春英胡海燕
Owner 北京航天飞腾装备技术有限责任公司
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