地空导弹武器装备RMS论证参数体系研究

通过对地空导弹武器装备RMS(可靠性、维修性、保障性)参数存在的问题进行分析,提出了RMS参数的选取原则,并建立了地空导弹武器装备RMS参数体系,为装备可靠性、维修性、保障性论证奠定了基础,该体系的建立有助于提高武器装备战备完好性、任务成功性,减低使用维修人员和保障资源费用。     

作战飞机可靠性与维修性仿真模型

通过故障树分析建立了作战飞机仿真逻辑关系。在修正线性同余法的基础上获得了随机数模型。在各设备故障发生状态和修复状态识别的基础上,建立了可靠性维修性仿真模型,确定了作战飞机在仿真过程中的工作状态,并根据故障模式影响分析预计了设备故障对作战飞机的影响。最后以F/A-18为例进行可靠性维修性仿真,获得了实时的故障信息和修复信息,验证了仿真模型的可行性。     

基于战备完好率的军用飞机维修费用需求确定方法

军用飞机维修费用需求与战备完好率要求密切相关,为保持飞机一定的战备完好率水平,必须投入一定的维修费用。维修费用投入多,则维修设备齐全,维修人员维修能力高,维修备件充足,飞机故障修复时间短,战备完好率高;维修费用投入少,会造成维修设备短缺,设施破旧,维修人员培训不到位,维修备件供应不足等各种问题,直接影响战备完好率水平。     

舰空导弹系统可靠性维修性对训练的影响

以舰空导弹武器系统远洋训练为研究背景,分析了舰空导弹武器系统可靠性、维修性对训练的影响.提出了可靠性、维修性对训练影响的具体指标,通过建立模型和仿真计算,在理论和应用上分析了航空导弹武器系统可靠性、维修性对训练的影响,得到了仿真应用结果并基于可靠性、维修性提出了对舰空导弹系统训练使用的建议.     

基于系统效能的可靠性维修性指标确定方法

为了使航空装备可靠性、维修性指标研究工作更加符合作战需求,在明确了效能及系统效能概念的基础上,结合系统效能评估模型E=ADC提出了基于系统效能的可靠性、维修性指标定量要求,并用图形体现。同时,定量分析了使用可用度、可信度及系统效能增长对可靠性、维修性指标的影响。     

鱼雷贮存战备完好率模型

为了评估鱼雷综合特性参数鱼雷贮存战备完好率,分析了国军标中基本模型,对照鱼雷寿命剖面,指出基本模型在具体鱼雷装备中应用存在的不足;通过对鱼雷寿命剖面中的基层级维修的深入分析,综合考虑贮存可靠度、故障检测率、鱼雷故障修复概率与备件满足率,给出了一个LRU故障、多个相同LRU故障以及多个不同LRU故障时的战备完好率模型。并通过计算验证了该模型的有效性。     

武器装备可靠性维修性保障性发展研究

武器装备的可靠性、维修性和保障性(R&M&S,包括测试性和安全性)是提高武器装备战备完好性和出动强度的基础,也是改善武器装备快速出动能力和机动性的有力保证。文章简要回顾了可靠性、维修性和保障性的发展历程,分析了现状,提出了R&M&S向着综合化、实用化、信息化、仿真化、智能化、微观化和军民两用化方向发展的趋势。     

未来武器装备可靠性维修性保障性发展趋势

武器装备的可靠性、维修性和保障性(R&M&S,包括测试性和安全性)是提高武器装备战备完好性和出动强度的基础,也是改善武器装备快速出动能力和机动性的有力保证。简要回顾了可靠性、维修性和保障性的发展历程,分析现状,判断未来,提出了R&M&S向着综合化、实用化、信息化、仿真化、智能化、微观化和军民两用化方向发展的趋势。     

基于动力学建模的装备自主保障系统性能仿真

自主保障是未来装备战场保障的重要发展趋势。论文以飞机发动机为对象,通过引入技术贡献率参数,建立其自主保障体系的动力学模型,并利用Vensim软件进行仿真分析,结果表明,自主保障体系在提高战备完好率、减少维修人员、降低维修费用和缩短保障时间方面具有明显优势。论文提出的方法为定量设计和评估其它装备自主保障体系提供了一种有效途径。     

面向任务的导弹测试性需求分析与指标确定

针对当前缺乏科学合理的理论和方法确定导弹系统级测试性指标的现状,提出一种面向任务需求的测试性指标确定方法.将导弹任务剖面划分为贮存、出库、部署和发射四个阶段,并提出各个阶段相应的测试需求;分别建立基于贮存可用度、战斗准备任务成功率、部署战备完好率和发射任务成功率为性能要求的测试性需求子模型,给出各个性能指标与测试性参数...     

Supercritical carbon dioxide as a new working medium for pneumatic launch: A theoretical study

Compared with the conventionally gaseous or liquid working media, the specific internal energy of supercritical carbon dioxide (SCD) is higher at the same temperature and pressure, and the critical temperature of carbon dioxide is close to room temperature, making SCD a potential new working medium for pneumatic launch. To analyze the feasibility of this conception, an analytical model of a pneumatic catapult is established on basis of the conservations of mass and energy. The model consists of a high-pressure chamber and a low-pressure chamber connected by multiple valves, and there is a movable piston in the low-pressure chamber that can push an aircraft to accelerate. The effects of the launch readiness state of SCD in the high-pressure chamber, the initial volume of the low-pressure chamber and the valve control on the movement of the aircraft are analyzed. It is found that there is a restrictive relation between the temperature and pressure of the launch readiness state of SCD, i.e., there is a maximum allowable launch readiness pressure when the launch readiness temperature is fixed. If this restrictive relation is not satisfied, the working medium in the low-pressure chamber will drop to its triple point within a few milliseconds, leading to a launch failure. Owing to this restrictive relation, there is an optimal launch readiness state of SCD with the highest working capacity for any allowable launch readiness temperature. The pressure of the low-pressure chamber will decrease significantly as the initial volume increases, leading to a decreased acceleration of the aircraft. The ac-celeration can be controlled below a critical value by a designed sequential blasting technique of multiple valves. The calculated results show that a 500 kg aircraft can be accelerated from 0 to 58 m/s in 0.9 s with 36 kg of carbon dioxide. This research provides a new technique for the controllable cold launch of an aircraft.     

军用飞机可用度概念模型及仿真

使用可用度是军用飞机战备完好性的重要度量标准.运用传统的解析法计算使用可用度有其弊端.以军用飞机使用及维修保障过程中各个系统要素为基础建立了使用可用度概念模型;根据概念模型运用仿真软件Extend建立了仿真模型.仿真结果表明模型运行稳定可靠,模型中各模块算法合理有效,实现了模型解算目标,可信度高.从而为飞机可用度研究提供了一种新方法.     

A stochastic air combat logistics decision model for Blue versus Red opposition

Technologically advanced aircraft rely on robust and responsive logistics systems to ensure a high state of operational readiness. This paper fills a critical gap in the literature for combat models by closely relating effectiveness of the logistics system to determinants of success in combat. We present a stochastic diffusion model of an aerial battle between Blue and Red forces. The number of aircraft of Blue forces aloft and ready to be aloft on combat missions is limited by the maximum number of assigned aircraft, the reliability of aircraft subsystems, and the logistic system's ability to repair and replenish those subsystems. Our parsimonious model can illustrate important trade‐offs between logistics decision variables and operational success.     

Scheduling prowler training

The U.S. Navy Prowler aircraft is designed for electronic surveillance and countermeasures. In this paper, we describe the problem of scheduling Prowler crew training, and we present two integer programming models to solve it. The first model maximizes the number of aviators trained above 75% in each mission area, subject to the available number of flights, over a single month. The second model distinguishes peacetime from mobilization, and minimizes the number of flights done in mobilization subject to the available number of flights in peacetime. Our models distinguish different types of crew and allow more than one qualification to be earned on a given flight. We give numerical results using real data, comparing our results to the actual readiness of a squadron. We found that crew readiness of Prowler squadrons can be increased by 10%, simply by better scheduling. © 2003 Wiley Periodicals, Inc. Naval Research Logistics 50: 289–305, 2003.     

Minimizing reductions in readiness caused by time-phased decreases in aircraft overhaul and repair activities

The Navy is often required to conduct personnel planning studies, A recent study on the assessment of effects of personnel reductions at the various aircraft Overhaul and Repair Activities (O & Rs) of the Bureau of Naval Weapons was carried out by one of the writers of the present paper. The methodology was systematic but relied on informal, judgmental decision procedures rather than on formal models incorporating optimization. Later study of the problem resulted in the approach described herein. The paper addresses this question: How can a personnel reduction in the Navy's aircraft O & Rs be distributed among activities with minimum reduction in readiness? A two-stage procedure involving linear programming models is developed. Solutions involve either extensions of aircraft overhaul cycles or a combination of such extensions with reductions in aircraft inventories.     

导弹装备战备完好性评估模型

针对当前对导弹战备完好性水平缺乏系统性评估,给导弹装备管理决策带来极大困难,难以适应当前转型建设导弹装备保障要求的问题,在对现役导弹装备任务剖面分析的基础上,对影响导弹战备完好性的重要参数使用可用度进行了研究,给出了基于可用性理论的导弹装备使用可用度评估方法和模型,根据部队导弹装备服役的相关信息,对该模型进行了评估验证,经验证,该方法可有效地分析导弹使用可用度,研究结论对于提升导弹装备战备完好性具有一定的借鉴意义。     

基于作战任务的多机种故障备件需求模型

通过分析战时故障备件的需求特点,对备件的工作时间进行讨论,改进了传统的单机故障备件需求模型。根据多机种协同作战任务的不同,引入备件工作运行比的概念,在考虑飞机是否战损的前提下,建立了基于作战任务的多机种故障备件需求模型。算例分析证明了模型的有效性。     

基于改进主成分分析法的装备战备水平评估研究

为了科学、合理地评估装备战备水平,构建了装备战备水平评估指标体系,并提出了基于改进的主成分分析法的装备战备水平评估模型及算法。改进的算法不仅消除了指标量纲和数量级的影响,还能包含原始数据的全部信息,在原始变量转变为主成分过程中,反映了主成分权数的计算综合评价值,在指标权重选择上克服了主观因素的影响,客观反映了各指标因素间的现实关系。并通过引入实例,证明该方法实现了更加快捷、直观地对部队装备战备水平进行评估,有利于正确地引导部队装备战备建设的方向。     

飞机运动态势对航空深弹入水点散布影响分析

航空自导深弹具有结构简单、可靠性高、不受水文条件限制等特点,而且还具有自导捕获和跟踪目标能力,对于提高航空兵部队反潜能力具有重要作用。反潜机投放高度、投放速度等运动态势关系到使用航空自导深弹对目标实施准确打击。针对航空自导鱼雷攻潜实际过程,建立其入水点的散布误差模型和空中弹道模型,并仿真分析反潜机投弹高度、投弹速度对航空自导深弹入水点的影响。