Control method of cooperative multi-missile combat

A technology of multiple missiles and control methods, applied in the field of guidance

Active Publication Date: 2018-06-15
BEIJING INSTITUTE OF TECHNOLOGYGY
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

[0004] The purpose of the present invention is to solve the problem of simultaneously enhancing the defense penetration capability and the target strike capability during multi-missile coordinated operations

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  • Control method of cooperative multi-missile combat
  • Control method of cooperative multi-missile combat
  • Control method of cooperative multi-missile combat

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Embodiment Construction

[0075] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0076] At present, in the field of multi-missile cooperative combat research, how to control each missile to simultaneously hit the target from different directions and specified angles in three-dimensional space is an important issue to improve the missile's defense penetration capability and enhance the missile's ability to strike the target . In the present invention:

[0077] As shown in Figure 1, first introduce the concept of virtual leader missiles, and assume that the virtual leader missiles fly vertically and laterally using the enhanced proportional guidance law; Set the angle to adjust the missile-to-target distance, so that the missile-to-target distance can track the missile-to-target distance of the virtual leader missile, so as to obtain the coordinated guidance law that can make multiple missiles attack the target at the same...

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Abstract

The invention discloses a control method of a cooperative multi-missile combat. Multiple missiles can be controlled to simultaneously strike a static or moving object with specified falling angles from different directions in a three-dimensional space, so that a breakthrough probability of the missiles and a striking ability on the object are greatly improved, and the object is saturation-attackedomnidirectionally. The method can be applied to multiple types of missiles, not only can be used for attacking a fixed object with a high value point, but also can be used for attacking the moving object, and has higher robustness for various interference types due to low computation complexity and high computation efficiency of an algorithm different from a traditional optimized algorithm used for on-line trajectory optimization; and the control method of the cooperative multi-missile combat has the characteristics of flexibility in application and stronger functions, and has a wide militaryapplication prospect.

Description

technical field [0001] The invention relates to a method for controlling the attack time and attack angle of multiple missiles in coordinated operations in three-dimensional space, and belongs to the field of guidance technology. Background technique [0002] With the continuous development of anti-missile technology, in the modern battlefield, the combat capability of a single missile is greatly limited. If multiple missiles can cooperate in combat——from different directions and hit the target at a specified angle at the same time, it will be greatly improved. Enhancing the missile's defense penetration capability and its ability to strike targets will also be the direction of future development of the missile weapon system. [0003] If it is required that multiple missiles can hit the target at the same time from different directions at a specified angle, it is necessary to constrain the attack angle and attack time of the missiles at the same time, and design a guidance l...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F42B15/01
Inventor 王晓芳王紫扬林海
Owner BEIJING INSTITUTE OF TECHNOLOGYGY
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