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Route planning method of multi-wave missile launching vehicle

A missile launch and path planning technology, applied in the field of transportation, can solve problems such as low utilization rate of reloading area, increased possibility of enemy attack, road node conflicts, etc.

Active Publication Date: 2018-12-18
SHAANXI UNIV OF SCI & TECH
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  • Claims
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AI Technical Summary

Problems solved by technology

If there is no reasonable planning for the path of the launch vehicle during the execution of the mission, the overall exposure time of the launch vehicle will be longer, increasing the possibility of being attacked by the enemy. Secondly, there may also be road node conflicts and the use of reloading areas. Low rate and other issues
[0004] In order to solve such problems, a large number of scholars have carried out research and analysis, but most of them only consider the single wave of missile launches, or optimize the road path under simple structural constraints.

Method used

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Embodiment Construction

[0052] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments, but the present invention is not limited to these embodiments.

[0053] The troops accept the strike mission requirements and need to meet the mission requirements while minimizing the overall exposure time of the launch vehicle. There are K different types of launching vehicles, and they are distributed in different standby areas. The salvo task requires that all launching vehicles of each wave arrive at the launching node to complete the strike task uniformly. Fill, and then go to the next launch node, repeat the above process, and the multi-wave strike mission is completed. Coexistence of Z throughout the combat zone i reprint area, F j transmitting nodes and J k Road nodes, two launching vehicles can be parked in each reloading area, but the reloading operation cannot be completed at the same time, and the working time of a singl...

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Abstract

The invention discloses a route planning method of a multi-wave missile launching vehicle. The method comprises the following steps: using a model established and a Floyd algorithm, respectively calculating the shortest route from each standby region to each missile launching node and route length; selecting w routes from several planned optimal routes and taking the selected routes as travellingroutes of the missile launching vehicle of a first wave, finding out the longest route from the selected w routes and then dividing the longest route by speed of the missile launching vehicle on a normal road to obtain maximum exposure time, namely, gradually completing route planning from the standby region to each missile launching node. The method provided by the invention can effectively solvea problem of route planning of the multi-wave missile launching vehicle and obtain the overall optimal route plan, can play an important role in data support of decision making of a military commandcenter, is beneficial for improving military task completion rate and enhancing overall fighting ability of troops.

Description

technical field [0001] The invention belongs to the technical field of transportation, and in particular relates to a path planning method for a multi-wave missile launching vehicle. Background technique [0002] Since the 21st century, with the advancement of science and technology and the changes of the times, the military warfare system has also changed from traditional mechanized warfare to current information warfare. Among information-based weapons, missiles have the advantages of large attack power, wide attack range, high attack accuracy, fast attack speed, and certain intelligence. Important position. But this also makes the enemy increase the destruction and interception of missiles. How to ensure that our army can quickly and effectively complete the target strike and improve its own survival rate when performing tasks is the focus of the current problem to be solved. [0003] In the actual battlefield, the launch vehicle loaded with the launch device is first p...

Claims

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Application Information

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IPC IPC(8): G01C21/20
CPCG01C21/20
Inventor 栾飞闫树江耿薇王航石冰洁陈梦瑶
Owner SHAANXI UNIV OF SCI & TECH
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