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1、2012-01题录英译集*基于弹上总线的导弹装备测试性设计方法胥辉旗，田燕妮，陈望达(海军航空工程学院科研部，山东 烟台 264001)摘要：为克服传统测试方法在测试数字电路板时的技术障碍，提出基于弹上总线及边界扫描的弹上设备机内自测试设计方案。在介绍IM总线(module test and maintenance bus，TM Bus)和边界扫描的基础上，论述系统测试性设计的基本概念，搭建测试试验系统，并对系统测试性设计概念和主要考核指标进行演示、验证。结果表明：该设计能简化导弹的测试流程，提高导弹武器系统的可靠性、维修性和测试性。关键词：导弹；测试性设计；机内测试；边界扫描Design f
2、or Testability of Missile Weapon Equipment Based on Missile Data BusXu Huiqi, Tian Yanni, Chen Wangda(Dept. of Scientific & Research, Naval Aeronautic & Astronautic University, Yantai 264001, China)Abstract: To overcome the technology barriers of the traditional test method in testing digital circui
3、t board, put forwards a new design scheme of missile equipment built-in self-testing based on missile data bus and boundary scan. Discuss the basic concept of system testing by introduce of the module test and maintenance bus (TM Bus) and boundary scan. A test system is designed to illustrate the co
4、ncept and test the main indicators of design for testability (DFT). Performance testing indicates that the design can simplify testing process and improve the reliability, maintainability and testability of missile weapon system.Key words: missile; design for testability; built-in test; boundary sca
5、n*小型无人直升机活塞式发动机建模技术徐志鑫1，曾国贵2，严峰2，祖家奎1(1. 南京航空航天大学自动化学院，南京 210016；2. 中国直升机设计研究所无人机部，江西 景德镇 333000)摘要：针对传统的无人直升机发动机研究方法存在的问题，提出一种新的活塞式航空发动机系统建模方案。结合旋翼系统的特性，利用叶素理论对旋翼桨叶进行分析，分别建立了发动机功率特性模型和旋翼的负载模型，根据发动机的动力学特性得到发动机的转速，并通过Matlab仿真和试车台试验进行验证。仿真试验结果证明：该模型合理可行，能够满足无人直升机的仿真控制要求。关键词：无人直升机；活塞发动机；建模；旋翼；负载Modelin
6、g Technique of Piston Engine System for Small Unmanned HelicopterXu Zhixin1, Zeng Guogui2, Yan Feng2, Zu Jiakui1(1. College of Automation Engineering, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China;2. Unmanned Aircraft Vehicle Division, China Helicopter Research & Developmen
7、t Institute, Jingdezhen 333000, China)Abstract: For the problems of traditional research methods of unmanned helicopter engine, a new modeling method of piston aircraft engine system was proposed. Combining with the characteristics of rotor system, blade element theory is applied to analyze rotor bl
8、ades. Then engine power characteristics model and rotor load model were established. According to the dynamics of engine, engine speed is calculated. Finally, Matlab simulation and ground test stand testing were carried out to verify the control performance. Simulation results show that the model is
9、 reasonable and feasible and meets the control requirements of unmanned helicopter simulation. Key words: unmanned helicopter; piston engine; modeling; rotor; load*战时飞机部件损坏率分析张作刚1，翟胜路1，王彦2(1. 海军航空工程学院青岛分院航空装备保障指挥系，山东 青岛 266041；2. 海军航空工程学院兵器科学与技术系，山东 烟台 264001)摘要：为更加准确地预测现代战争条件下的飞机部件损坏率，提出一种基于可靠性和兰彻斯
10、特方程的飞机部件损坏率预测方法。着眼于影响战时飞机部件损坏的内外部因素，在飞机部件中引入当量面积的概念，在飞机能够生存的前提下，根据各个部件受伤对飞机的生存影响，运用兰彻斯特方程和可靠性工程理论计算该部件的战伤概率，通过定性分析和定量计算，得出战时飞机部件的损坏率，并举例进行验证。实例结果证明：该方法将经验计算和模拟计算相结合，满足了未来作战维修保障精确化的需要。关键词：损坏率；兰彻斯特方程；当量面积；部件战伤率Damages Rate Analysis of Aircraft Part in WarfareZhang Zuogang1, Zhai Shenglu1, Wang Yan2(1.
11、 Dept. of Aeronautical Equipment Support & Command, Qingdao Branch, Naval Aeronautical & Astronautical University, Qingdao 266041, China;2. Dept. of Ordnance Science & Technology, Naval Aeronautical & Astronautical University, Yantai 264001, China)Abstract: For the precise estimation of aircraft par
12、t damages in warfare, Lanchester Equation and reliability project theory are used to solve the problem. Focusing on the internal and external factors that affect the aircraft part damages, introduce the equivalent area into aircraft part, puts forward the estimation method of aircraft part damage ba
13、sed on reliability and Lanchester Equation by qualitative analyze and quantitative calculation, and illustrates with an example. This method combined the experience calculation with the analog calculation, can meet the need of accurate maintenance support in future warfare. Key words: damage rate; L
14、anchester equation; equivalent area; the damage of aircraft part*基于跑道灯光的计算机视觉辅助无人机着陆李飞1，谭乐祖2，唐亮3(1. 海军航空工程学院控制工程系，山东 烟台 264001；2. 海军航空工程学院指挥系，山东 烟台 264001；3. 海军航空兵第92514部队，山东 烟台，264001)摘要：针对夜间无人机着陆时标准跑道的灯光会加重图像处理的难度问题，提出一种利用跑道灯光辅助着陆的机器视觉方法。该方法参考标准跑道灯光设置，提取跑道灯光直线特征，对EPnP方法进行扩展，将直线特征表示成跑道平面上3个控制点的加权形式
15、，利用奇异值分解的方法求出控制点在相机坐标系中的坐标，最后使用正交化方法解算出无人机相对于跑道的位置和姿态，为无人机着陆提供了引导信息。仿真结果表明：在距机场距离较远时，该方法能有效地引导其自主着陆。关键词：视觉；着陆；位姿估计；EPnP方法Computer Vision Assisted UAV Landing Based on Runway LightsLi Fei1, Tan Lezu2, Tang Liang3(1. Dept. of Control Engineering, Naval Aeronautical & Astronautical University, Yantai 2
16、64001, China;2. Dept. of Command, Naval Aeronautical & Astronautical University, Yantai 264001, China;3. No. 92514 Unit of Naval Air Force, Yantai 264001, China)Abstract: In order to assist landing of unmanned aircraft vehicle (UAV), a vision-based method is proposed, which makes use of runway light
17、s. Simple configure of runway lights is set up refer to standard runway lighting. EPnP method is extended to line based pose estimation after the lines made up of runway lights are extracted. Each line is expressed as a weighted sum of three control points, and the camera coordinates of the control
18、points can be estimated through singular value decomposition (SVD). Then, with the orthogonalization method, the position and attitudes of UAV are calculated, to provide the navigation information for UAV landing. Simulation results show that the algorithm proposed is accurate in the earlier stage o
19、f landing.Key word: vision; landing; pose estimation; EPnP method*高威力、高分子粘结炸药与双锥金属药型罩药柱压制成型技术谢建湘(湖南云箭集团有限公司工程技术中心，湖南 怀化 419503)摘要：为提高子弹战斗部破甲威力，开展了对子弹药柱采用新型高威力、高分子粘结炸药(聚黑-2炸药)与双锥金属药型罩(以下简称药型罩)整体压制成型技术研究，利用金属射流的高密度来提高子弹战斗部破甲威力。针对采用双锥金属药型罩的高分子粘结炸药药柱压制成型过程中的安全性、药柱易于膨胀等技术难点，对压药模具、压药工艺方法、技术参数、工艺设计等4个方面进行分
20、析，并进行了工艺试验。抽样数据表明：该技术既保证了生产安全，又提高了药柱成型质量。关键词：聚黑-2炸药；药柱；药型罩；回弹性；压药压力；保压时间High Power, High Polymer Bonded Explosives and Bipyramid Metal Liners Grain Pressing TechnologyXie Jianxiang(Engineering Technology Center, Hunan Vanguard Group Co., Ltd., Huaihua 419503, China)Abstract: In order to improve the
21、bullet warhead sunder armor, and carried out the power subsidiary ammunition with new high strength, column polymer binder explosives (poly black-2 explosives) and double cone metal medicine type cover (hereinafter referred to as medicine type cover) overall pressure molding technology research, usi
22、ng the high density of the metal jet to improve the bullet warhead sunder armor power. According to adopt double cone metal type of polymer binder medicine cover explosives column pressure molding process of drug safety, explosive easy to expansion and so on technical difficulties, and on the pressu
23、re medicine mould, pressure medicine process, technical parameters, process design and analysis, and the technology experiment. Sample data shows that the effect is satisfied, not only ensure the production safety, and also to improve the explosive forming quality.Key words: poly black-2 explosives;
24、 grain; medicine type cover; elasticity; pressure drug pressure; dwell time*高效毁伤注装药工艺技术孙家利，王秋雨，夏克祥，郝英华(中国兵器工业集团123厂技术部，黑龙江 齐齐哈尔 161046)摘要：为加强我国炮兵弹药的高效毁伤能力，对大口径弹高效毁伤注装药工艺技术进行研究。介绍改性B炸药性能、注装药工艺试验、检验和生产性分析，并经多批生产进行了可行性验证。生产实际证明：我国大口径炮弹注装改性B炸药后，综合威力提高40%以上，具有一定的军事效益。关键词：高效毁伤；改性B炸药；注装药工艺；综合威力High Efficie
25、ncy Damage Melt-Loading Process TechnologySun Jiali, Wang Qiuyu, Xia Kexiang, Hao Yinghua(Technical Department, No. 123 Factory of China North Industries Group Corporation, Qiqihaer 161046, China)Abstract: In order to strengthen high efficiency damage capability of artillery ammunition in our countr
26、y, research on melt-loading process technology of large caliber ammunition had been carries out. The properties of improved composition B, melt-loading process test, inspection and production analysis were introduced, and feasibility verification was carried through many batch productions. Productio
27、n practice proves that composite power increased 40% above after improved composition B changed for large caliber artillery ammunition, it has definite military efficacy.Key words: high efficiency damage; improved composition B; melt-loading process; composite power*基于点图的作战任务时间协同一致性检验方法姚剑，朱延广，曹星平，王维
28、平(国防科学技术大学信息系统与管理学院，长沙 410073)摘要：针对作战计划制定过程中任务时间协同一致性的问题，提出基于点图推断并校验时间的方法。构建描述作战任务时间协同关系的点图模型，通过顶点聚合运算、顶点折叠运算和顶点时间运算3种基本运算进行检验，给出了作战任务时间协同一致性检验方法，并结合测试案例对方法的有效性进行验证。验证结果表明，该方法能有效地检验作战任务时间协同的一致性。关键词：作战任务；时间协同一致性；点图；时间推理Verify the Operational Task Temporal Collaboration Consistency Based on Point Grap
29、hYao Jian, Zhu Yanguang, Cao Xingping, Wang Weiping (School of Information System & Management, National University of Defense Technology, Changsha 410073, China)Abstract：The task of verifying the operational task temporal collaboration consistency in military planning is researched based on the poi
30、nt-graph (PG), and a method based on PG to cope with temporal reasoning is designed. Build a PG model to describe operational task temporal collaboration, verify the operational task temporal by point-unification, point-folding and point-time calculation, and a consistency verifying algorithm is giv
31、en. Finally, an example is present to illustrate the feasibility and effectiveness of above method. Key words：operational task; temporal collaboration consistency; point graph; temporal reasoning*基于直觉三角模糊数向量投影的多属性决策方法王安，周存宝(解放军炮兵学院应用数学系，合肥 230031)摘要：针对直觉三角模糊数向量投影引发的多属性决策问题，提出了一种属性权重确知、且属性值以直觉三角模糊数形式
32、给出的多属性决策方法。从向量投影的角度出发，给出2个直觉三角模糊数向量之间投影的算法，进而利用各个方案的加权属性值在模糊理想解上的投影值大小对方案进行排序，并用实例进行验证。实验结果表明：该方法简洁明了、思路清晰，具有一定可行性和实用性，易于在实际应用中推广。关键词：直觉三角模糊数；投影；多属性决策；偏好Method for Multi-Attribute Decision-Making Based on the Projection of Intuitionistic Triangular Fuzzy Number VectorsWang An, Zhou Cunbao(Dept. of A
33、pplied Mathematics, Artillery Academy of PLA, Hefei 230031, China)Abstract: Aiming at the multiple attributes decision making problem caused by intuitionistic triangular fuzzy number vectors projection, a method is proposed in which the attribute weights are completely known and the attribute values
34、 are in the form of intuitionistic triangular fuzzy numbers. From the angle of vector projection, the arithmetic of projection between two intuitionistic triangular fuzzy number vectors is given, then the alternatives are ranked by using the projection of the weighted attribute values of every alter
35、natives on the fuzzy positive ideal point. In the end a numerical example is given out. The results show that this method is simple, clear and easy for use, and the work has an important applied value for multiple attributes decision making.Key words: intuitionistic triangular fuzzy numbers; project
36、ion; multiple attributes decision making; preferences*车辆野战维修装备编配数量建模和仿真舒华1，柴怡2，赵劲松1，高永刚2，刘凯3(1. 军事交通学院装备保障系，天津 300161；2. 军事交通学院研究生管理大队，天津 300161；3. 中国人民解放军71282部队装备部，河南 洛阳 471023)摘要：为了提高军队车辆的装备保障整体效能，对车辆野战维修装备的编配进行研究。在分析影响编配数量的各种因素的基础上，确定车辆野战维修装备编配的维修任务量和单车维修作业能力，建立面向任务的车辆野战维修装备编配数量模型，并经过Matlab软件进行仿
37、真验证。验证结果表明：该模型可为车辆装备的合理化、科学化保障提供了辅助决策支持。关键词：车辆野战维修装备；编配数量；建模；仿真 Allocation Amount Modeling and Simulation of Vehicle Battlefield Maintenance EquipmentShu Hua1, Chai Yi2, Zhao Jinsong1, Gao Yonggang2, Liu Kai2(1. Dept. of Equipment Support, Academy of Military Transportation, Tianjin 300161, China;2.
38、 Administrant Brigade of Postgraduate, Academy of Military Transportation, Tianjin 300161, China;3. Equipment Department, No. 71282 Unit of PLA, Luoyang 471023, China)Abstract: In order to improve military vehicle equipment support integrant efficiency, the paper studies allocation of vehicle battle
39、field maintenance equipment. By analyzing influential factors of allocation amount, it determines maintenance mission of allocating vehicle battlefield maintenance equipment and the maintenance capability of a single vehicle, established the allocation model based on mission. The model was validated
40、 by Matlab simulation. The model can provide assistant decision support for rationalization and scientific vehicle equipment support.Key words: vehicle battlefield maintenance equipment; allocation number; modeling; simulation*海军航空兵飞行团转场飞机选择模型齐玉东1，闫晓斌2，谢晓方1(1. 海军航空工程学院兵器科学与技术系，山东 烟台 264001；2. 海军航空工程
41、学院训练部，山东 烟台 264001)摘要：为解决目前飞行团制定转场飞机使用计划时存在的问题，设计一种海军航空兵飞行团转场飞机选择模型。根据各种影响因素合理确定使用寿命战备储存量，结合一些转场飞机选择规则，使用混合整数规划的方法，对飞行团转场飞机选择方法进行改进，优化出转场飞机，并对所建立飞机选择模型进行实例验证。实验结果证明：该模型能合理制定飞机使用计划，科学调度飞机，保证转场期间飞机的有效使用，具有较高的应用价值。关键词：机动转场；飞机寿命；飞机选择；混合整数规划Aircraft Selecting Model for Naval Aviation Regiment Transportat
42、ionQi Yudong1, Yan Xiaobin2, Xie Xiaofang1(1. Dept. of Ordnance Science & Technology, Naval Aeronautical & Astronautical University, Yantai 264001, China;2. Training Department, Naval Aeronautical & Astronautical University, Yantai 264001, China)Abstract: When air regiment plan to select aircrafts f
43、or transportation some problems arisen, in order to solve them, this paper established and validated an aircraft selection model with mixed integer programming (MIP) on the base of some aircraft selection rules and a reasonable storage life with various factors. Experimental results show that this m
44、odel has a high application value for the rational aircraft usage programs, scientific control of the aircraft, ensure the effective use of aircraft on the transportation period. Key words: motor transportation; aircraft life; aircraft selection; MIP*属性权重不确知的区间直觉模糊群决策方法陈之宁1，周存宝2，王安3(1. 解放军陆军军官学院基础部数
45、学教研室，合肥 230031；2. 解放军陆军军官学院五系41队，合肥 230031；3. 解放军陆军军官学院五系42队，合肥 230031)摘要：针对区间直觉模糊多属性群决策中属性权重信息事先不能确知的问题，提出一种基于区间直觉模糊混合平均算子(IIFHA)区间直觉模糊多属性群决策方法。给出属性权重确定的方法，列出群决策计算方法与步骤，并通过实例进行验证。结果表明：该方法是正确、有效的，能为相关人员提供一定的参考。关键词：得分矩阵；IIFHA算子；权重；群决策Method of Interval Intuitionistic Fuzzy Group Decision-Making Based
46、 on the Unknown Attribute WeightsChen Zhining1, Zhou Cunbao2, Wang An3(1. Staff Room of Mathematics, Dept. of Basic Theories, Military Academy of PLA, Hefei 230031, China;2. No. 41 Team, No. 5 Department, Military Academy of PLA, Hefei 230031, China;3. No. 42 Team, No. 5 Department, Military Academy of PLA, Hefei 230031, China)Abstr
