摘要：【中文】本发明公开了一种超低空作战条件下的多支路引信探测距离通道压缩的方法，通过综合利用弹体的姿态信息、引信的高度支路探测信息和目标探测支路的天线方向图，实时计算出目标探测支路的距离压缩范围。相比以往的引信探测计算方法，该方法可在充分利用现有探测信息的基础上，实现设计的优化，不需要增加其它硬件探测设备，不增加系统硬件设计的复杂性，在避免引信探测到海面回波信号引起早炸的同时最大限度的发挥了引信对目标的探测能力，实现对目标的有效探测和杀伤。 【EN】The invention discloses a method for compressing multi-branch fuze detection distance channels under an ultra-low altitude combat condition, which calculates the distance compression range of a target detection branch in real time by comprehensively utilizing the attitude information of a projectile body, the height branch detection information of a fuze and the antenna directional diagram of the target detection branch. Compared with the conventional fuze detection calculation method, the method can realize the optimization of design on the basis of fully utilizing the existing detection information without adding other hardware detection equipment or increasing the complexity of system hardware design, furthest plays the detection capability of the fuze on the target while avoiding the early explosion caused by the detection of sea echo signals by the fuze, and realizes the effective detection and killing of the target.

摘要：【中文】本发明公开了一种通用复杂引战系统仿真的方法及系统，所述方法包括：根据多个型号引战系统的特点，确定通用复杂引战系统仿真的总体架构，基于所述总体架构，选择不同的天线方向图、引信灵敏度曲线配置文件，设置引信波长、信号处理周期、采样点位置与采样数量以设计不同类型引信；按照给定格式设置相关参数形成战斗部配置文件，以设计多种战斗部；通过选择不同的弹道与目标库中的目标类型，利用相应的引战配合数学模型计算不同引战系统在各种交会条件下对各种典型目标的毁伤情况，以进行引战系统仿真。本发明的优点是：实现简单，通过模块化和通用化设计，实现了只需使用者按照给定格式设置相关参数的配置文件便可实现不同的引战系统设计与仿真。 【EN】The invention discloses a method and a system for simulating a universal complex war introduction system, wherein the method comprises the following steps: determining the general architecture of the simulation of the universal complex fuze warfare system according to the characteristics of a plurality of models of fuze warfare systems, selecting different antenna directional diagrams and fuze sensitivity curve configuration files based on the general architecture, and setting fuze wavelength, signal processing period, sampling point position and sampling quantity to design different types of fuzes; setting relevant parameters according to a given format to form a configuration file of the warhead so as to design various warheads; by selecting different trajectory and target types in the target library, the damage conditions of different missile systems to various typical targets under various meeting conditions are calculated by utilizing corresponding missile and mathematic models, so as to simulate the missile and war systems. The invention has the advantages that: the method is simple to realize, and different warfare system designs and simulations can be realized by setting the configuration files of the related parameters according to the given format by a user through modularization and universalization design.

摘要：【中文】本发明提出了一种多支路引信目标探测建模的方法,解决以往方法不能对多支路复杂引信以及超低空作战进行设计和仿真的问题。本发明构建了多支路天馈系统模型，地面/海面回波模型和引信目标回波模型。满足复杂多支路引信与引战配合设计的需求，能够数字化再现真实作战场景，具有很高的置信度和实用性。具有成本低廉、试验周期短、可满足在不同地面和海情下多种交会姿态下针对多种目标的引战系统设计、仿真、评估与分析的需求。 【EN】The invention provides a method for detecting and modeling a multi-branch fuse target, which solves the problem that the conventional method cannot design and simulate a multi-branch complex fuse and an ultra-low-altitude battle. The invention constructs a multi-branch antenna feeder system model, a ground/sea echo model and a fuze target echo model. The requirement of complex multi-branch fuse and fuse fighting matching design is met, the real fighting scene can be digitally reproduced, and high confidence coefficient and practicability are achieved. The method has the advantages of low cost and short test period, and can meet the requirements of design, simulation, evaluation and analysis of a war-inducing system aiming at various targets under various meeting postures on different grounds and sea conditions.

摘要：【中文】本发明提出了一种超低空作战条件下的战斗部破片飞散轨迹计算的方法,通过构建在弹目相对速度坐标系内由于空气阻力的作用的战斗部破片飞散轨迹变模型，有效解决了在超低空作战条件下战斗部破片命中目标的精度问题，并可针对大规模仿真计算进行精度设置，满足不同计算精度和计算规模的平衡。相比传统的战斗部破片飞散轨迹计算的方法，该方法能够准确仿真评估超低空作战条件下的引战配合设计、引战系统设计和武器系统作战效能。 【EN】The invention provides a method for calculating the fragment flying trace of a warhead under the condition of ultra-low-altitude operation, which effectively solves the precision problem of target hitting of the fragment of the warhead under the condition of the ultra-low-altitude operation by constructing a variable model of the fragment flying trace of the warhead due to the action of air resistance in a relative speed coordinate system of a bullet, can perform precision setting aiming at large-scale simulation calculation, and meets the balance of different calculation precision and calculation scale. Compared with the traditional warhead fragment flying trajectory calculation method, the method can accurately simulate and evaluate the fighting cooperation design, the fighting system design and the weapon system fighting efficiency under the condition of ultra-low-altitude fighting.