Multiple missile collaborative ballistic planning method to deal with penetration

A multi-missile and missile technology, applied in aerospace ballistics and guidance, and aviation fields, can solve problems such as missile errors, achieve the effect of small radar detection threats and improve comprehensive combat effectiveness

Active Publication Date: 2018-03-20
NAT UNIV OF DEFENSE TECH
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Problems solved by technology

Although some existing research methods can achieve multi-missile coordinated attack targets, the research objects are mainly for low-speed aircraft, ...

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  • Multiple missile collaborative ballistic planning method to deal with penetration
  • Multiple missile collaborative ballistic planning method to deal with penetration
  • Multiple missile collaborative ballistic planning method to deal with penetration

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Embodiment Construction

[0069] In order to make the technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, not to limit the present invention.

[0070] The embodiment of the present invention proposes a multi-missile cooperative trajectory planning method for penetration, including the following steps:

[0071] Step 1. According to the radar equation, establish a radar threat quantitative model to describe the threat of the radar detection area to the missile.

[0072] Assuming that within the radar detection area, the threat coefficient of any position is proportional to the signal-to-noise ratio of the position, that is:

[0073] R k ∞S / N (1)

[0074] Where: R k is the threat coefficient; S / N is the signal-to-noise ratio of the radar.

[00...

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Abstract

The invention provides a multiple missile collaborative ballistic planning method to deal with penetration. The method comprises the specific steps that step 1, based on the radar equation, a radar threat quantification model is established to describe the threat of a radar detection area to a missile; step 2, a collaborative control model is established, the collaborative control model comprisesa collaborative time control model and a collaborative angle control model; step 3, a collaborative attack problem is converted into a nonlinear optimal control problem which is solved based on a hp-self adaptive Radau pseudospectral method, which means at one moment of the flight, the remaining flight time of each missile is determined, whether or not a collaboration is necessary, if necessary, the time for the collaborative attack is calculated and the missile to be adjusted is determined, and the collaborative ballistic planning is conducted on the missile needs to be adjusted. According tothe multiple missile collaborative ballistic planning method, multiple missiles attacking a target on the same attacking time and with the same attacking angle is ensured; meanwhile, the radar detection threat is smallest during the flight, and the comprehensive combat effectiveness is effectively improved.

Description

technical field [0001] The invention relates to a coordinated ballistic planning method that realizes attack time and attack angle coordination when controlling multi-missile cooperative operations, and satisfies the minimum radar threat, and belongs to the technical field of aviation and aerospace ballistics and guidance. Background technique [0002] Future warfare will be an offensive and defensive confrontation between combat systems, especially the confrontation between the attack system based on precision-guided weapons and the increasingly strengthened modern defense system. In a complex battlefield environment, radar, as a main detection method of the enemy, poses a strong threat to the penetration of missiles. [0003] In order to achieve effective penetration and improve comprehensive combat effectiveness, the U.S. military took the lead in proposing the concept of coordinated operations and achieved a series of research results. [0004] At present, multi-missile...

Claims

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Application Information

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IPC IPC(8): G06F17/50F41G7/00
CPCF41G7/007G06F30/20
Inventor 葛健全许强强杨涛陶烨张青斌丰志伟赵创业汤志威王亮
Owner NAT UNIV OF DEFENSE TECH
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