美国海军无人机系统的发展现状、趋势及关键技术

简要介绍了美国海军无人机系统的目前装备情况及发展计划,论述了其发展趋势及关键技术。     

基于H_∞飞控系统重构方法研究

将飞机的重构控制问题转化为H∞控制问题,并运用H∞方法对故障时的飞行控制系统进行了重构,运用残差方法实现了故障的检测、隔离。仿真结果表明,所设计的重构控制律在舵面受损的情况下能够使飞机保持良好的飞行性能。     

电磁气动阀四机集成设计

针对某空间飞行器对轨控发动机控制阀体积及重量的要求,统筹考虑气液路供应、4台发动机、氧化剂及燃料贮箱的安装要求,设计了新颖的电磁气动阀四机集成结构。经仿真分析及试验实测,结果表明:电磁气动阀四机集成结构具有设计巧妙、性能优良的特点。     

飞行器轨迹控制若干术语探讨

分析比较了领航、指挥引导、导航、制导、载机导引和导弹导引等飞行器轨迹控制中常用的若干术语,明确了这些术语的区别与联系.依据不同条件下不同飞行器轨迹控制的具体问题,提出了规范使用这些术语的建议.     

JJG 860-2015《压力传感器(静态)检定规程》浅析

介绍了JJG 860-2015《压力传感器(静态)检定规程》的主要变化,就检定设备的选择、特殊压力传感器的检定方法等对规程进行浅析,结合测试实例论述了新增传感器零点漂移和周期稳定性两个性能指标的必要性,并对规程的进一步完善提出了建议。     

国外舰载飞机着舰进近适配性评估技术研究

通过对国外舰载飞机在着舰进近下滑中的操纵需求分析,提出舰载飞机着舰进近适配性的评估要求。在评估要求的基础上针对飞机在进近适配性方面相关的特性给出相应的飞行试验方法和分析方法,初步建立舰载飞机着舰进近适配性评估技术和方法。     

High-efficiency aircraft antiskid brake control algorithm via runway condition identification based on an on-off valve array

The aircraft antiskid braking system is an important hydraulic system for preventing tire bursts and ensuring safe take-off and landing. The brake system adjusts the force applied on the brake discs by controlling the brake pressure. Traditional aircraft antiskid braking systems achieve antiskid performance by controlling the braking pressure with an electrohydraulic servo valve. Because the pilot stage of an electrohydraulic servo valve is easily blocked by carbonized hydraulic oil, the servo valve would become a dangerous weak point for aircraft safety. This paper proposes a new approach that uses an on-off valve array to replace the servo valve for pressure control. Based on this new pressure control component, an efficient antiskid control algorithm that can utilize this discontinuous feature is proposed. Furthermore, the algorithm has the ability to identify the runway circumstances. To overcome the discontinuity in the process of using an on-off valve array, the Filippov framework is introduced. The conditions of convergence of the system are also discussed. The results of the digital simulations and the hardware-in-the-loop (HIL) braking experiments are used to verify the efficiency and stability of the proposed control algorithm. The method also proves that the on-off valve array can replace the servo valve perfectly as a new type of antiskid braking pressure control component.     

第十一届新加坡航展印象

简要介绍了第十一届新加坡航展的参展情况。通过参观访问深感军民用发动机市场竞争十分激烈。GE、PW、RR等公司均积极地参与了中国ARJ21新支线喷气客机选发的竞争,我国“新舟60”首次参展引起了国内外同行的关注。     

现代战机导引系统及其关键技术

阐述了现代战机导引系统的功能、结构与工作方式.基于对导弹制导等相关问题的深入研究,以及对战机导引的特点分析,阐述了战机导引控制律设计中应当解决的关键技术与研究途径,包括远距导引、近距导引和机动导引不同阶段的特点、捕获域的定义与计算方法、战机导引律研究特点及其基本工作模态.本研究可为新一代战机导引系统的研制提供参考.