ID 原文 译文
24525 交叉眼干扰是单脉冲雷达最有效的干扰方式之一，增益是衡量交叉眼干扰性能的重要指标。 Cross eye jamming is one of the most effective jamming methods for monopulse radar, and cross eye gainis an important index to measure the performance of cross eye jamming.
24526 本文在两源反向交叉眼干扰（TRCJ, Two source Retro-directive Cross-eye Jamming）和多源线阵反向交叉眼干扰（LMRCJ, Linear array Multi-source Retro-directive Cross-eye Jamming）增益模型的基础上，以 4源线阵反向交叉眼干扰为例，对相同幅值比下 LMRCJ的增益最大值进行了推导，提出了 LMRCJ整体相位容限计算方法，综合考虑 LMRCJ不同环路之间的相位控制方式、幅相波动以及平台回波等因素，对比分析了 LMRCJ和 TRCJ的增益值和幅相容限。 Based on the gain models of two source retro-directive cross-eye jamming (TRCJ) and linear array multi-source retro-directive cross-eye jamming (LMRCJ), the maximum gainvalue of LMRCJ under the same amplitude ratio is deduced by taking the cross eye interference of 4-source linear array as an example, and the calculation method of overall phase tolerance of LMRCJ is proposed. Considering the phase control mode between different loops of LMRCJ, amplitude phase fluctuation and platform echo, the gain value and amplitude compatibility limit of LMRCJ and TRCJ are compared and analyzed.
24527 仿真结果表明：不考虑平台回波时，在相同的幅值比下，TRCJ 的增益最大值不低于 LMRCJ 的增益最大值，且增益值高时 TRCJ 的相位容限比 LMRCJ的相位容限更宽松； The simulation results show that, without considering the platform echo, the maximum gain of TRCJ is not lower than that of LMRCJ under the same amplitude ratio, and the phase tolerance of TRCJ is more relaxed than that of LMRCJ when the gain is high;
24528 当 LMRCJ 和 TRCJ 的幅相控制能力相同且均较弱时，LMRCJ 的增益值高于 TRCJ 的增益值； when the amplitude and phase control capabilities of LMRCJ and TRCJ are the same and weak, the gain of LMRCJ is higher than that of TRCJ;
24529 考虑平台回波时，在高干信比（JSR, Jam-to-Signal Ratio）下，LMRCJ 和 TRCJ 的增益及相位容限规律与隔离平台回波时的一致。 when considering the platform echo, the gain and phase tolerance of LMRCJ and TRCJ are consistent with those of isolating platform echo athigh JSR.
24530 论文研究可以为交叉眼干扰机的工程设计提供指导。 The paper can provide guidance for the engineering design of the cross-eye jammer.
24531 针对民营商业运载火箭“双曲线一号”高可靠、低成本、快响应的要求，设计了一种自定义高速串行总线架构的高集成度箭载综合电子系统。 Aiming at the requirement of high reliability, low cost and fast response of the private commercial launch vehicle "Hyperbola-1", a high-integrated launch vehicle integrated modular avionics is designed.
24532 描述了综合电子系统的任务需求、各功能模块原理组成、叠板结构设计、实时操作系统以及飞控软件等关键技术。 This paper describes the task requirements of integrated modular avionics, the principle composition of each function module, the structure design of laminated board, real-time operating system and flight control software.
24533 重点阐述了基于 Zynq处理器的主控模块最小系统及通讯接口设计、自定义高速串行总线架构设计。 Emphasis is given to the design of minimum system, communication interface of the main control module based on Zynq, and the design of custom high-speed serial bus architecture.
24534 随着双曲线一号首飞试验的成功，作为控制中枢的综合电子系统工作正常，满足民营商业运载火箭强实时性、高可靠性以及高精度控制等要求。 With the success of the first flight test of Hyperbola-1, integrated modular avionics, as a control center, works normally and meets the requirements of high real-time, high reliability and high precision control of private commercial launch vehicles.