ID 原文 译文
38446 然后,基于后悔函数将证据推理方法的权重求解问题转化为非线性多目标优化问题。 Then, based on regret function will be the weight of evidence reasoning method to solve the problem into a nonlinear multi-objective optimization problem.
38447 最后,采用萤火虫算法计算最优参数,确定最优评估模型并得到最终评估结果。 Finally, the optimal parameters are calculated by use of a firefly algorithm, and determine the optimal evaluation model and get the final evaluation results.
38448 算例分析结果表明,所提方法能够有效解决评估主观性强的问题,提高评估结果的准确度,对装备保障资源供给能力评估问题具有较好的适用性。 The example analysis results show that the proposed method can effectively solve the problem of assessing subjective strong, enhance the accuracy of evaluation results, the equipment support resources supply capacity evaluation has good applicability.
38449 地空导弹装备在高原开展训练时,面临众多具有随机性和模糊性特点的风险因素。 Surface to air missile equipment in plateau training, many have the characteristics of randomness and fuzziness of risk factors.
38450 针对该问题,结合高原环境以及地空导弹装备作战流程,分析了影响其高原训练安全的主要风险因素,构建了安全风险评估指标体系。 Aiming at this problem, combined with the plateau environment and surface-to-air missile combat process, analyzed the main risk factors affecting the safety of the altitude training, safety risk assessment index system is constructed.
38451 在模糊综合评价法的基础上引入云模型,通过云模型的熵和超熵反映风险的随机性和模糊性,提出了基于云模型的地空导弹装备高原训练安全风险评估方法。 On the basis of the fuzzy comprehensive evaluation method into the cloud model, through the cloud model of entropy and entropy reflects the randomness and fuzziness of the risk, based on cloud model is put forward in the surface to air missile equipment altitude training safety risk assessment methods.
38452 最后,通过一个算例分析验证了该方法的实用性。 Finally, through a case analysis verify the practicability of the method.
38453 研究结果可为风险控制提供参考。 The results can provide reference for risk control.
38454 针对单脉冲雷达检测跟踪协同干扰状态的双隐身飞机编队时,角度跟踪误差性能难以合理评价的问题,首次建立了基于侧双机编队平飞航迹的隐身飞机协同闪烁非相参干扰模型,经过相同航迹下编队姿态的解算,获取闪烁干扰模型下的编队动态雷达散射截面序列, For tracking monopulse radar detection, collaborative interference of the state of the double stealth aircraft fleet, Angle tracking error performance is the problem of reasonable evaluation, for the first time based on flight of lateral double stealth aircraft flying track synergy blink of coherent interference model, through the same track of attitude of formation, the interference model flashes for dynamic radar scattering cross section sequence formation,
38455 结合双机闪烁干扰模型下单脉冲雷达角度跟踪特点,推导得出与双机编队闪烁干扰相适应的单脉冲雷达角度误差跟踪模型,以最小干扰有效诱偏角为实时参变量对闪烁干扰模式下雷达角度跟踪误差性能变化的程度作出了评价。 combined with the double machine monopulse radar Angle tracking characteristics of blinking jamming model derived with the formation of two blinking jamming adaptive monopulse radar Angle tracking error model, with the minimum interference effectively induced Angle for real-time radar Angle of blinking jamming mode parameter assesses the extent of the tracking error performance changes.