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王玉茜 , 曹亚杰 , 佘晓琼 , 等 . 美军杀伤网概念研究及对我防空作战装备体系的启示 [J ] . 现代防御技术 , 2023 , 51 ( 6 ): 1 - 8 . DOI: 10.3969/j.issn.1009-086x.2023.06.001 http://doi.org/10.3969/j.issn.1009-086x.2023.06.001 DARPA寻求从杀伤链转向杀伤网，意图利用信息网络构建高度分散的杀伤网，形成难以预测的杀伤链。美空军在试验旗体系下开展“橙旗”“翠旗”和“黑旗”试验，探索杀伤网概念的落地应用。首先，围绕杀伤网作战概念，阐述杀伤网与杀伤链的内涵与差异；其次，理清DARPA“自适应跨域杀伤网”项目的发展背景，分析其基于电子商务“供应商—消费者”框架的架构设计，总结其“跨域杀伤网协商与实例化的实时推理分析”软件针对项目关键技术的演示验证情况；再次，从作战管理、体系架构、安全通信、基础设施、标准规范等方面提出构建杀伤网所需的关键技术；最后，瞄准构建未来防御作战弹性杀伤网，从技术角度给出建设我防空作战装备体系的建议。

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陈登 , 陈楚湘 , 周春华 . 基于OODA环的杀伤网节点重要性评估 [J ] . 兵工学报 , 2024 , 45 ( 2 ): 363 - 372 . DOI: 10.12382/bgxb.2022.0623 http://doi.org/10.12382/bgxb.2022.0623 基于网络信息体系的联合作战中,破坏敌杀伤网、降效敌杀伤体系作战效能,要求能够识别敌杀伤网中关键节点。基于OODA环理论及杀伤链概念建模,利用节点删除法,通过网络作战能力及网络循环效率两项指标的下降程度评估杀伤网节点的重要性,克服传统评估方法在指标计算中存在冗余的问题,提高评估精度。采用该方法评估某作战演练中敌方杀伤网节点的重要性,精准识别指挥决策节点的枢纽作用,验证方法的有效性,并对杀伤网节点的重要性进行评估排序,为选择进攻要点提供依据。

CHEN D , CHENG C X , ZHOU C H . Importance evaluation of kill network nodes based on OODA loop [J ] . Acta Armamentarii , 2024 , 45 ( 2 ): 363 - 372 . (in Chinese) DOI: 10.12382/bgxb.2022.0623 http://doi.org/10.12382/bgxb.2022.0623 In joint operations based on the network information system, paralyzing the enemy kill network and reducingthe operational effectiveness of enemy kill system requires the ability to identify the key nodes in the enemy kill networks. Kill network modeling based on OODA loop theory and kill chain operational concept, this paper uses the node deletion method to evaluate the importance of kill network nodes through the decline degree of network operational capability and network cycle efficiency, so as to overcome the problem of redundancy in the index calculation of traditional evaluation methods and improve the evaluation accuracy. This method is used to evaluate the importance of enemy kill network nodes in the operation drill, which accurately identifies the pivotal role of command and decision nodes to verify the effectiveness of the method, and which evaluates and ranks the importance of kill network nodes to provide a basis for selecting attack nodes.

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丁伟 , 明振军 , 王国新 , 等 . 基于正向解析式和多目标博弈优化算法的复杂装备体系优化设计方法 [J ] . 兵工学报 , 2024 , 45 ( 6 ): 1974 - 1990 . DOI: 10.12382/bgxb.2023.0031 http://doi.org/10.12382/bgxb.2023.0031 针对复杂装备体系(Complex Equipment System-of-systems, CES)优化设计中指标变量多、仿真依赖性强、易陷入局部最优的问题,提出一种基于正向解析式和多目标博弈理论(Multi-Objective Game Theory, MOGT)优化算法的CES优化设计方法。为提升CES优化设计的可解释性,构建任务级—能力级—装备级的评估指标体系;在此基础上,基于装备机理和效用函数表征装备评估指标与作战能力之间的正向映射关系,并利用相邻优属度熵权法计算各指标权重;通过正向解析式与约束条件建立多目标优化模型,并采用MOGT优化算法获得最佳优化结果。以某作战推演平台中防空攻防想定为例,开展算例评估与验证分析。研究结果表明,该方法能够实现CES中最优设计方案的求解,可显著提高设计效率和降低设计成本,为下一代装备发展论证、设计评估和作战试验提供了基础性工作。

DING W , MING Z J , WANG G X , et al . Optimization design method of complex equipment system-of-systems based on forward analytical formula and MOGT optimization algorithm [J ] . Acta Armamentarii , 2024 , 45 ( 6 ): 1974 - 1990 . (in Chinese) DOI: 10.12382/bgxb.2023.0031 http://doi.org/10.12382/bgxb.2023.0031 For the problems of many index variables, strong simulation dependence and being easy to fall into local optimum in the optimization design of complex equipment system-of-systems (CES), an optimization design method of CES based on forward analytical formula and multi-objective game theory (MOGT) optimization algorithm is proposed. In order to improve the interpretability of the CES optimization design, evaluation index systems among task-level, capability-level and equipment-level are constructed. On this basis, the positive mapping relationship between the evaluation performance index and the combat capability is characterized based on the equipment mechanism and utility function, and the weight of each index is calculated by the adjacent priority degree entropy weight method. A multi-objective optimization model is established by using the forward analytical formulas and constraints, and the MOGT optimization algorithm is used to obtain the best optimization results.The air defense scenario in an operation deduction platform is taken as an example for the example evaluation and verification analysis. The results show that the proposed method can realize the solution of the optimal design scheme in the CES, which can significantly improve the design efficiency and reduce the design cost, and provide the basic work for the development demonstration, design evaluation and combat test of the next generation equipment.

徐公国 , 段修生 , 单甘霖 , 等 . 基于多目标局部变异-自适应量子粒子群优化算法的复杂地形多传感器优化部署 [J ] . 兵工学报 , 2018 , 39 ( 11 ): 2192 - 2201 . DOI: 10.3969/j.issn.1000-1093.2018.11.013 http://doi.org/10.3969/j.issn.1000-1093.2018.11.013 对复杂地形下的多传感器部署问题进行研究，提出了基于多目标局部变异-自适应量子粒子群优化（LM-AQPSO）算法的多传感器多目标优化部署方法。该方法对复杂地形进行多属性网格建模，给出了传感器探测模型和优化目标。引进局部变异和参数自适应策略对量子粒子群优化算法进行改进，并提出了基于LM-AQPSO的多目标Pareto最优解集优化算法。考虑多目标部署需求，构建了基于Pareto最优解集的多传感器优化部署模型。仿真实验结果表明：相对于经典的改进非支配排序遗传算法，所提算法优化的Pareto最优解有着更好的收敛性和分布性，且寻优时间更短；所提模型能有效解决多目标多传感器部署问题，并能同时提供更多的决策方案。

XU G G , DUAN X S , SHAN G L , et al . Optimization deployment of multi-sensors in complex terrain based on multi-objective LM-AQPSO algorithm [J ] . Acta Armamentarii , 2018 , 39 ( 11 ): 2192 - 2201 . (in Chinese)

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CHEN Z W , HONG D P , CUI W W , et al . Resilience evaluation and optimal design for weapon system of systems with dynamic reconfiguration [J ] . Reliability Engineering and System Safety , 2023 , 237 : 109409 .

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周健 , 龚春林 , 粟华 , 等 . 飞行器体系优化设计问题 [J ] . 航空学报 , 2018 , 39 ( 11 ): 222223 . DOI: 10.7527/S1000-6893.2018.22223 http://doi.org/10.7527/S1000-6893.2018.22223 针对传统的飞行器设计与体系（SOS）设计相互独立造成的飞行器实际作战效能不足的问题，对同时考虑飞行器与体系耦合设计的飞行器体系优化设计问题展开研究。首先，根据体系工程（SOSE）原理给出了耦合飞行器设计与体系结构设计的飞行器体系优化设计问题的基本概念与通用数学定义；其次，基于多层体系架构，构建了飞行器体系设计优化模型，提出了包含问题定义、体系架构建模、学科建模、优化求解4个步骤的通用建模求解流程；最后，以巡飞/精确打击武器协同作战为例，构建了面向任务成本最低、时间最短的协同作战体系最优化问题并对其进行优化求解。与先设计飞行器后设计体系结构的解耦设计结果对比表明，解耦优化设计忽略了体系结构与飞行器的强耦合特征，无法最优化体系效能；耦合优化设计能够获得体系效能最大化的飞行器设计方案。

ZHOU J , GONG C L , SU H , et al . Optimal design problem of system of systems of flight vehicle [J ] . Acta Aeronautica et Astronautica Sinica , 2018 , 39 ( 11 ): 222223 . (in Chinese) DOI: 10.7527/S1000-6893.2018.22223 http://doi.org/10.7527/S1000-6893.2018.22223 To address the insufficient actual operational effectiveness of the flight vehicle caused by the independence between the traditional flight vehicle design and the System of Systems (SOS) design, and the defects of manual iteration, the optimal coupling design of flight vehicle and system of systems is studied in this paper. First, based on the principle of System of Systems Engineering (SOSE), this paper presents the basic concept and general mathematical definition of the optimal design of the flight vehicle system of systems combined SOS architeclure design and flight vehicle design. Then, based on the multi-level system of systems architecture, a model for the optimal design of the flight vehicle system of systems is built, and a general modeling and solving process for such a problem is proposed, which includes the definition of the problem, its architecture modeling, its discipline modeling, and its optimization of problem solving. Finally, taking LAM/PAM cooperative weapon system combat application case as an example, an optimization task of pursing the shortest attacking time and the lowest cost is built and solved. Calculation results show that the design result of the decoupling design mode, which designs the flight vehicle first and then the system of systems, cannot meet the demand of combat operations, but the design result of the coupling design method can complete the combat mission much better and produce flight vehicle conceptual design schemes that can maximize the effectiveness of the system of systems.