Method for controlling attack angle and attack time of multiple missiles

Abstract

The invention provides a method for controlling the attack angle and the attack time of multiple missiles. With the adoption of the method, the attack angle and the attack time of the multiple missiles can be accurately controlled. The method comprises the following steps: arbitrarily selecting one missile from multiple missiles to serve as a master missile; constructing a virtual sphere by taking a target as a sphere center and taking distance between the master missile and the target as a radius; defining the residual missiles as slave missiles; selecting virtual points for each slave missile on the surface of the virtual sphere, wherein direction of a connection line of each virtual point and the target is a preset ideal attack angle corresponding to the slave missile; and by controlling a slave missile movement locus, approaching and tracking a virtual point locus, so that control of the attack angle and the attack time of multiple missiles is realized. The method for controlling the attack angle and the attack time of the multiple missiles is realized by approaching and tracking the virtual point corresponding to the slave missile by the slave missile, so that the attack angle and the attack time of the slave missiles can be controlled without appointing ideal attack time for each slave missile in advance.

Description

technical field [0001] The invention relates to a method for controlling the attack angle and attack time of multiple missiles, which belongs to the field of guidance technology. Background technique [0002] With the rapid development of science and technology, the capabilities of missile defense systems have been continuously enhanced. In many cases, a single missile operation can no longer meet the requirements of the battlefield. The coordinated operation of multiple missiles has become more and more important. In order to improve the lethality of missile coordinated operations, there are usually requirements for the attack angle, and in order to achieve saturation attack, there are requirements for the attack time. If multiple missiles can simultaneously attack targets from different angles, the strike capability of the missiles will be greatly enhanced. [0003] The technology of simultaneous control of missile attack angle and attack time at home and abroad is still ...

AI Technical Summary

Problems solved by technology

[0004] The technical problem to be solved by the present invention is to overcome the difficulties of the above-mentioned prior art, and provide a method for controlling the attack angle and attack time of multiple missiles without specifying the ideal attack time in advance and without limiting the target motion state

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