ID 原文 译文
9604 首先引入威力场的概念并构建载机威力势模型。 First of all introduced the concept of force field and build the aircraft power potential model.
9605 其次以战场指挥员对目标装备性能的主观认知及载机的威力为基础,利用模糊层次分析法对不确定信息条件下的目标威力进行评估。 Next to the battlefield commander subjective cognition on the property of the target equipment and the aircraft power as the foundation, using the fuzzy analytic hierarchy process (ahp) to evaluate target power under the condition of uncertain information.
9606 然后利用参照依赖效应计算载机与目标间各项能力的收益-损失值,进而应用前景理论给出最佳的接敌队形选择方法。 Then use reference to depend on the carrier aircraft and the target effect calculate the ability of profit/loss value, and the application prospect of theory to give the best answer the enemy formations selection method.
9607 最后对此方法进行了仿真验证。 Finally for the simulation of this method.
9608 结果表明,该方法能够在不确定信息条件下对接敌队形进行有效选择。 Results show that this method is able to under the condition of uncertain information docking enemy formation effectively.
9609 首先分析了旋转平台控制误差对惯导系统(inertial navigation system,INS)调制效果的影响; First analyzed the rotating platform control error of inertial navigation system (inertial navigation system, INS) modulation effect;
9610 然后建立了旋转平台的数学模型,结合旋转调制误差抑制效果对控制性能的要求,提出了一种自抗扰和滑模变结构相结合的复合旋转控制方法。 And then established the mathematical model of the rotating platform, combining with the rotating modulation error inhibition effect to the requirement of control performance, this paper proposes a self immunity and combined composite rotation of the sliding mode variable structure control method.
9611 该方法充分利用了滑模变结构控制快速减小误差的优势和自抗扰控制的精确估计能力,并设计了融合策略。 This method can make full use of the sliding mode variable structure control fast advantage to lower the error and the immunity control ability of accurate estimation and design of the fusion strategy. ‭
9612 仿真和实验结果表明,相比于传统PID控制方法,本文方法减小了旋转平台转速控制误差,且使反向角度超调误差和调节时间都减小了50%以上,提高了旋转调制惯导系统的性能。 Simulation and experimental results show that compared with the traditional PID control method, the method reduces the rotation error of speed control platform, overshoot and reverse Angle error and adjust time is reduced by more than 50%, improve the performance of the rotating modulation inertial navigation system.
9613 超长基线双基机载雷达杂波的空时分布特性不仅严重依赖于双基雷达构型,也取决于地球曲率引入的波束覆盖问题。 Long baseline double-base space-time distribution characteristics of airborne radar clutter rely heavily on double-base radar configuration not only, also depends on the earth curvature is introduced into beam coverage problem.