System-dynamics-based balance design method for weapon support system

A system dynamics and system balance technology, applied in the direction of instruments, calculations, special data processing applications, etc., can solve problems such as failure to consider balance problems, low resource utilization efficiency, etc., and achieve the effect of facilitating balance analysis and improving transshipment efficiency

Active Publication Date: 2016-08-03
CSSC SYST ENG RES INST
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  • Abstract
  • Description
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AI Technical Summary

Problems solved by technology

[0009] As a subsystem of the aviation comprehensive support system, the weapon support system is currently designed in accordance with the above-mentioned design method. Because the balance problem is not considered, the resource utilization efficiency is low

Method used

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  • System-dynamics-based balance design method for weapon support system
  • System-dynamics-based balance design method for weapon support system
  • System-dynamics-based balance design method for weapon support system

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Embodiment Construction

[0027] The method of the present invention takes system balance as the goal, and the scheme for modeling and analyzing the balance performance of the weapon support system is as follows: firstly, the boundary of the weapon support system is determined, and the change of the quantity of lifts and ammunition is defined using system dynamics modeling, while other parts of the system use discrete Event simulation modeling; then establish the system dynamics model of the elevator and ammunition quantity change, and establish the discrete event simulation model of other parts of the system; then couple the system dynamics model and the discrete event model to obtain the overall model of the weapon support system; finally based on The obtained overall model is simulated and analyzed, the balance performance simulation result is obtained, and the possible imbalance points in the weapon support system are identified. The specific process is as follows: figure 1 shown.

[0028] Step 1: ...

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Abstract

A system-dynamics-based balance design method for a weapon support system comprises the following steps: firstly, determining the boundary of the weapon support system, and making clear that system dynamics is used for modeling of a lift and the change of ammunition quantity and discrete event simulation is used for modeling of other parts in the system; then building a system dynamics model of the lift and the change of ammunition quantity, and building a discrete event simulation model of other parts of the system; coupling the system dynamics model and the discrete event model to obtain an integral model of the weapon support system; finally, performing simulation analysis based on the obtained integral model to obtain a balance performance simulation result and to identify probable unbalance points in the weapon support system. The system-dynamics-based balance design method can analyze transport of ammunition and assembly resource utilization ratio in the system, find out bottleneck and unbalanced links in the process and improve the resource utilization efficiency of the system.

Description

technical field [0001] The invention relates to a balance design method of an aircraft carrier weapon support system. Background technique [0002] The integrated aviation support system is the first-level system of an aircraft carrier, with command and support of carrier-based aircraft as its main task, including tower flight command, maintenance support, ship surface supply support, ammunition supply, take-off and landing support, carrier-based aircraft deployment, maintenance task support As well as functions such as aviation operations, command and management, it is a complex large-scale system with a very tight combination of "man-machine-environment", which directly affects the dispatch and recovery capabilities of carrier-based aircraft. The complexity of the aviation integrated support system itself determines the difficulty of its design, and it also increases the difficulty of analyzing the system performance. [0003] At present, the design methods of aviation in...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G06F17/50
CPCG06F30/367
Inventor 李昊华刘广朱梦妮李海旭
Owner CSSC SYST ENG RES INST
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