基于多尺度分布式融合估计的GPS/INS组合导航系统的研究

针对如何融合多传感器的数据、提高数据处理的可靠性和精度的问题,将基于模型的动态系统分析方法与基于统计特性的多测度信号变换方法相结合,提出基于Kalman滤波的多尺度分解与估计联合的多尺度分布式融合估计算法.该算法首先建立系统的动态方程和观测方程,再利用小波变换将数据在不同尺度上进行融合处理,归纳出该算法的实现步骤.最后通过组合导航系统的仿真验证算法的有效性,结果进一步证明了该算法能够有效地提高多传感器数据的处理精度.     

基于CDFRFT的离散LFM信号参数估计方法

文章根据LFM信号在置中分数傅里叶变换域产生尖峰的原理,提出了一种基于置中分数傅里叶变换的离散LFM信号参数估计算法,并对单LFM信号和双LFM信号进行了参数估计,实验结果表明算法具有较好的精确性。     

一种适用于飞机装配的新型随动定位器

在飞机机身等大部件位姿调整、对接及精加工等装配过程中,如何保持调整后的飞机部件位姿不变并对其进行可靠固持一直是个技术难题。为此,提出一种基于气浮和万向球座的机身部件随动固持方法。采用该方法进行随动固持的具体步骤：首先将与机身部件刚性连接的芯轴插入处于浮动状态的万向球座中,芯轴在进入浮动球体的过程中,球体可在上、下半球座之间进行任意转动;然后根据受力状态使球体和上、下半球座一起平动;芯轴完全进入浮动跟随装置之后,液压锁紧上、下半球座和球体,同时锁紧芯轴,在保证不改变飞机大部件位姿前提下实现对其可靠固持;将油压卸载就可以释放与机身部件连接的芯轴,使机身部件恢复到自由调姿状态。试验和应用分析表明,这种新的随动固持方法可以满足机身对接装配、精加工要求。     

用二次相关提高超声测风精度和噪声抑制性能

以超声测风为应用背景,对基于相关法的时延估计性能进行分析,指出其存在的问题。利用发射信号为已知这一先验信息,提出了二次相关估计时延的解决方法。仿真结果表明,在相同的信噪比下,与相关法相比,二次相关法能够利用先验信息,提高了时延估计的正确率,并能改善系统6dB以上的噪声抑制性能。最后,对二次相关法的运算量进行了分析,并分别以TI TMS320C5000系列DSP处理器和Ahera CycloneⅡ系列FPGA作为硬件平台,估计了该方法在这两种平台上的处理时间,得出了该方法可满足实时处理的结论。     

Conceptual design of near-space synthetic aperture radar for high-resolution and wide-swath imaging

Airborne synthetic aperture radar (SAR) has the capability of high-resolution, and spaceborne SAR has the capability of wide-swath. Inspired by recent advances in near-space defined as the region between 20 km and 100 km, this paper conceptually designed near-space vehicle-borne SAR. The near-space vehicle-borne SAR has the synthetical advantages of the satellite and airplane platforms. By placing SAR transmitter or receiver in near-space vehicles, many functions that are currently performed with satellites or airplanes could be performed in low cost way. These advantages make simultaneous high-resolution and wide-swath SAR imaging possible. As such, this paper focuses on the role of near-space vehicle for high-resolution and wide-swath SAR imaging, and deals with conceptual performance, as opposed to technological implementation. The concepts, models and processing algorithms are provided. To further suppress the azimuth ambiguities and extend swath width, multiple beams in azimuth is applied. Furthermore, an example near-space vehicle-borne SAR is designed. It is shown that the use of cost effective near-space vehicles can provide the solutions that were previously thought to be out of reach for remote sensing scientists and customers.     

五种智能算法解决最大割问题分析与比较

最大割问题（Max—eulProblem）是一个典型的NP难组合优化问题。文章采用遗传算法、分布估计算法、Hopfield网络方法、蚁群算法、粒子群算法等5种算法对最大割问题进行求解,并用标准的多个不同规模最大割测试数据进行测试,研究各参数对算法的影响,并比较各种算法的时间复杂度和空间复杂度。测试结果表明该五种算法虽然在执行效率上有差异,但都能较好的解决最大割问题。     

天地基联合多星定轨及精度分析

数据中继卫星和双星定位系统通常由2或3颗地球同步卫星和数颗近地卫星组成,这些系统所提供的“星-星”测量数据提出了多星同时定轨的需求。文章介绍了已知天基星星历定轨和未知天基星星历定轨的主要差别,建立了距离和观测量的测量模型,描述了多星同时定轨的技术难点,分析了整个系统的定轨精度。     

超视距多机协同空战目标分配算法

针对未来超视距条件下多机协同空战中的威胁估计与多目标分配,结合超视距空战特点,在综合考虑参战双方飞机性能、几何态势的基础上,提出了一种以参战双方飞机空战效能优势与当前态势优势的加权和为最终结果的超视距空战威胁估计的非参量法模型;在威胁估计的基础上,探讨了一种以空战优势函数为依据,多机之间相互配合、相互支援、协同作战过程的多目标分配算法,并进行了仿真.仿真结果证实了算法的有效性.      

基于偏最小二乘回归法的飞机总工时预测模型研究

从影响军用飞机生产制造工时的众多因素中提取出24个飞机总工时影响因素,采用统计学方法结合理论分析对此24个因素进行科学筛选,筛选出飞机最大起飞重量、最大速度、爬升率、最大过载、钛铝合金比例、复合材料与铝合金比例这6个关键影响因素。考虑偏最小二乘回归(PLS)法在处理小样本多元数据方面的优势,采用PLS法对飞机总工时进行预测,预测结果表明PLS预测模型平均检验误差约为10%。该模型在实际使用过程中,只需获得飞机性能指标和材料构成等少数设计参数即可在飞机产品生产制造前对飞机生产制造总工时进行宏观预测,具有参数少、物理意义明晰、操作简单、便于使用、准确率高等特点,可为缺乏详细设计信息和生产信息的飞机研制早期方案优选、设计优化或对其进行费用分析和成本控制、固定资产投资、安排生产计划等工作提供相对准确的飞机产品工时。     

Structural optimization for multiple structure cases and multiple payload cases with a two-level multipoint approximation method

This paper is to address structural optimization problems where multiple structure cases or multiple payload cases can be considered simultaneously. Both types of optimization problems involve multiple finite element models at each iteration step, which draws high demands in opti-mization methods. Considering the common characteristic for these two types of problems, which is that the design domain keeps the same no matter what the structure cases or payload cases are, both problems can be formulated into the unified expressions. A two-level multipoint approxima-tion (TMA) method is firstly improved with the use of analytical sensitivity analysis for structural mass, and then this improved method is utilized to tackle these two types of problems. Based on the commercial finite element software MSC.Patran/Nastran, an optimization system for multiple structure cases and multiple payload cases is developed. Numerical examples are conducted to ver-ify its feasibility and efficiency, and the necessity for the simultaneous optimizations of multiple structure cases and multiple payload cases are illustrated as well.