扩频谱相关自适应滤波技术的研究

被高速伪随机码调制的扩频信号,其伪随机码是具有随机编码信号特征的周期信号。所以,扩频信号应被建模为周期信号(循环平稳信号)。循环平稳信号与其信号的频移副本之间具有很强的谱相关性,充分利用这种谱相关性可以实现对窄带和宽带干扰的抑制。基于循环平稳理论和自适应滤波理论,提出了一种基于改进的LMS算法的扩频信号谱相关自适应滤波技术。这种变步长的谱相关自适应LMS滤波器能实现对窄带和宽带干扰的抑制,仿真结果证明了其有效性。     

A novel target detection approach based on adaptive radar waveform design

To resolve problems of complicated clutter, fast-varying scenes, and low signal-clutterratio (SCR) in application of target detection on sea for space-based radar (SBR), a target detection approach based on adaptive waveform design is proposed in this paper. Firstly, complicated sea clutter is modeled as compound Gaussian process, and a target is modeled as some scatterers with Gaussian reflectivity. Secondly, every dwell duration of radar is divided into several sub-dwells. Regular linear frequency modulated pulses are transmitted at Sub-dwell 1, and the received signal at this sub-dwell is used to estimate clutter covariance matrices and pre-detection. Estimated matrices are updated at every following sub-dwell by multiple particle filtering to cope with fast-varying clutter scenes of SBR. Furthermore, waveform of every following sub-dwell is designed adaptively according to mean square optimization technique. Finally, principal component analysis and generalized likelihood ratio test is used for mitigation of colored interference and property of constant false alarm rate, respectively. Simulation results show that, considering configuration of SBR and condition of complicated clutter, 9 dB is reduced for SCR which reliable detection requires by this target detection approach. Therefore, the work in this paper can markedly improve radar detection performance for weak targets.     

闪电防护铜网在航空复材制件VARI成型工艺中的树脂导流应用

复合材料在民机结构中的大量应用对航空复材制件的闪电防护提出了新的要求,与此同时,以VARI工艺为代表的复材液体成型技术愈发受到关注,常用导流网在VARI工艺中造成浪费也易引起质量问题,结合这两方面的需求,提出将闪电防护铜网用作导流介质,在表面应用类的航空复材制件的VARI成型工艺中,将铜网的闪电防护作用和树脂导流作用进行集成,并对闪电防护铜网在VARI工艺中的树脂导流作用进行了试验分析,研究了引入铜网导流后VARI制件的注胶情况、铜网层数对树脂渗透率的影响,以及制件最终成型效果和表面质量。本研究对于丰富复材VARI成型工艺技术手段,提升VARI工艺的综合经济性,进一步拓展VARI工艺在民机复材结构中的应用都具有积极意义。     

Cr,Al含量对铸造TiAl基合金显微组织的影响

为寻找细晶组织的铸造ＴｉＡｌ基合金，在Ｔｉ－４４Ａｌ（ａｔ－％）和Ｔｉ－４８Ａｌ（ａｔ－％）两种Ａｌ含量的二元合金中添加了３Ｃｒ和６Ｃｒ（ａｔ－％）。结果表明，Ｃｒ对铸态α＿２＋γ合金的晶粒大小无明显的影响，但通过热处理可显著细化晶粒。对Ｔｉ－４４Ａｌ－３Ｃｒ和Ｔｉ－４８Ａｌ－３Ｃｒ合金分别采用１１５０℃、１６８ｈ和１２００℃、２４ｈ处理可取得最佳的细化晶粒效果，而且４８Ａｌ合金热处理后可更容易获得细晶组织。Ｃｒ促进有序富Ｃｒ相β＿２的形成，该相或者与片状α＿２相共生，或者分布于γ相的晶界，阻碍γ相长大。Ｃｒ在β＿２、γ＿２和γ相中的溶解度依次减少，它主要取代γ和α＿２相中的Ｔｉ，因而随着合金中Ｃｒ量增加，γ和α＿２相中的Ａｌ／Ｔｉ比增加。Ｃｒ还促使γ相内形成孪晶。     

体积成形过程的模型跟随自适应控制

为控制热锻的生产过程和锻件的产品质量 ,应用体积成形过程的有限元数值仿真离线训练人工神经网络 (ANN) ,采用电学模拟方法 ,通过简单的模拟电路构造出复杂的ANN模型 ,完成了从体积成形过程到模拟电路之间的映射。模拟电路与自适应控制系统并联 ,构成了模型跟踪的自适应控制系统     

带副翼偏转的三角翼自由滚转运动数值模拟

 通过耦合求解非定常Euler/Navier-Stokes方程和单自由度滚转运动方程,对带副翼偏转的65°后掠角尖前缘三角翼WI1-SLE自由滚转运动进行了研究,Navier-Stokes方程的求解采用基于Spalart-Allmaras湍流模型的脱体涡模拟(DES)。在多块结构网格上,应用基于弧长的无限插值理论(TFI)生成变形网格,实现副翼偏转,而三角翼的滚转运动则通过网格的整体旋转实现。结果表明:Euler方程和DES方法均准确地模拟出了三角翼在滚转运动过程中存在的3个平衡位置。出现平衡位置的原因分别是:①流动对称性;②机翼左侧发生涡破裂的分离涡与右侧分离涡相互平衡使得滚转力矩为0,并且平衡位置仅与三角翼两侧涡强的差有关;③副翼偏转和左右机翼不对称分离涡涡强差产生的滚转力矩相互平衡。此外,滚转运动对副翼偏角幅值很敏感,幅值的微小改变会影响最终的平衡位置和向平衡位置运动的路径。     

Consensus disturbance rejection control of directed multi-agent networks with extended state observer

This paper investigates the consensus disturbance rejection problem among multiple high-order agents with directed graphs.Based on disturbance observers,distributed consensus disturbance rejection protocols are constructed in leaderless and leader-follower consensus setups.Different from the previous related papers,the consensus protocols in this paper are developed in a fully distributed fashion,relying on only the state information of each agent and its neighbors.Sufficient conditions are prov...     

NLR-7301高升力翼型绕流评估计算

探讨了在二维高升力多段翼型绕流计算中附面层网格采用各向异性三角形网格的技术。通过对经典的NLR-7301两段翼型绕流的计算,从数值计算角度评估了自研混合网格雷诺平均N-S方程求解软件对该类型附面层网格的解算能力。通过与确认试验数据对比,在附面层采用各向异性三角形网格进行二维高升力多段翼型绕流计算,其结果具有较高的可信度。在此基础上,采用同样策略,评估了多段翼型绕流计算中翼型后缘的几何处理、湍流模型选取等关键CFD要素对计算结果的影响。     

高速平板着水数值模拟

探索和揭示物体入水冲击的流体力学现象与机理对飞行器水上迫降问题的研究有重要的参考价值。对高速平板着水涉及到的复杂物理问题展开数值模拟,采用有限体积法求解非定常雷诺平均Navier-Stokes(URANS)方程和标准k-ε湍流模型,流体体积(VOF)模型捕捉水气交界面,整体动网格技术处理平板与水面的相对运动。在二维楔形体入水冲击的算例验证基础上,详细研究平板高速着水引起流体喷溅、射流、空气垫等现象和平板底面压力变化历程,结果表明:空气垫现象明显,俯仰角4°平板下表面出现规律的空气泡,10°时则不存在;平板下表面的水体沿壁面运动,当俯仰角为10°时,壁面水体的运动速度显著增加;在大俯仰角的情况下明显出现负压区。     

Adaptive formation control of quadrotor unmanned aerial vehicles with bounded control thrust

In this paper, the flight formation control problem of a group of quadrotor unmanned aerial vehicles (UAVs) with parametric uncertainties and external disturbances is studied. Unit-quaternions are used to represent the attitudes of the quadrotor UAVs. Separating the model into a translational subsystem and a rotational subsystem, an intermediary control input is introduced to track a desired velocity and extract desired orientations. Then considering the internal parametric uncertainties and external disturbances of the quadrotor UAVs, the priori-bounded intermediary adaptive control input is designed for velocity tracking and formation keeping, by which the bounded control thrust and the desired orientation can be extracted. Thereafter, an adaptive con-trol torque input is designed for the rotational subsystem to track the desired orientation. With the proposed control scheme, the desired velocity is tracked and a desired formation shape is built up. Global stability of the closed-loop system is proven via Lyapunov-based stability analysis. Numer-ical simulation results are presented to illustrate the effectiveness of the proposed control scheme.