基于重叠型区域分解的时域积分方程法

时域平面波算法可以降低时域积分方程的计算复杂度以及内存消耗,但是时域积分方程的阻抗矩阵的近场部分元素无法减少,内存消耗依然很大。提出了利用重叠型区域分解法降低时域积分方程的内存需求,通过采取划分子区域,利用特征基函数法降低阻抗矩阵规模的方法,降低了内存消耗。数值算例验证了重叠型区域分解法结合时域积分方程能有效地用于瞬态电磁散射问题的分析。     

短期免耕对黑土孔隙度的影响

对短期玉米免耕和秋翻处理对耕层黑土孔隙度的影响进行了分析。结果表明,耕作处理对土壤孔隙度影响较大,毛管孔隙和贮存孔隙在整个剖面内免耕均小于秋翻,但秋翻处理下的中小孔隙占有很大比例。两个处理之间的大孔隙数量相差很小,多在3%～8%之间。秋翻总孔隙度表现出表层和底层差异很大,而免耕孔隙分布相对均匀,且上下孔隙连通性较好。     

曲面薄壳有限元离散误差分析和修正方法研究

基于曲面薄壳几何/物理方程和有限元离散原理推导,揭示了壳单元离散方法特点、刚度矩阵误差产生机理和范数表示方法。以航空涡轮发动机测压探针为例,深入研究了利用协调平板壳单元、非协调平板壳单元、一次和二次实体退化壳单元等不同类型单元离散曲面薄壳时,应力计算误差影响因素及变化规律,综述了单元的适用条件。基于Boltzmann模型提出了应力计算结果修正通式,通过FORTRAN语言编程修正应力仿真结果和ANSYS二次开发语言APDL命令实现应力修正结果的读取和后处理,应力修正结果与理论解相对误差小于5%,满足曲面薄壳设计和稳定性分析应用要求。

Abstract：

Based on the geometric physical equations and deduction of discrete process of finite element for curved thin-walled structure,characteristics of shell elements for discretion and discrete error for element stiffness matrix were analyzed theoretically,and the norm expression of discrete error for element stiffness matrix was put forward.Then,as an illustration,a probe for detecting the pressure inside turboprops was meshed by curved thin-walled shell element,compatible flat shell element,incompatible flat shell element and 3D degenerated shell element,respectively,and the stress of the probe was numerically calculated by FEM.On the basis of solved results,the stress error was analyzed thoroughly,the influence factors on the error and the applying situations for different elements were determined.Finally,the general form of correctional function was put forward according to the Boltzmann model.The program developed with FORTRAN was used to correct the numerical results and the APDL commands inside ANSYS software were utilized to read and plot the correctional stress results.Through the correction,the discrete error can be reduced within 5% that satisfies the requirement of application for structural design and stability analysis.     

基于IMU/GPS的性能导航方法研究

利用直角坐标系与大地坐标系之间的关系,将状态方程直接采用经纬度描述,GPS测量数据与电子地图上的经纬度相匹配,建立了混合模型,给出了一种新的GPS与IMU融合估计方法,提高了重复定位精度,更方便地实现组合导航系统功能。采用GPS和IMU装置进行了地面车辆试验和实际飞行试验,说明了模型和方法的适用性。

Abstract：

A mixed model was established and a new fusion estimation method for GPS and IMU was proposed through the relationship between the Cartesian coordinate system and the ground coordinate system,and the state equation described by the latitude and longitude directly,and the GPS measurement data and electronic map matched to the latitude and longitude.The provided method has improved the repeatability positioning accuracy and more easily integrated navigation system functions.The ground and actual flight were tested to illustrate the applicability of the model and method with GPS and IMU device.     

基于反馈线性化的船舶自动舵模糊滑模控制

针对船舶航向自动舵控制系统的非线性数学模型,应用基于微分几何的反馈线性化方法,将原非线性系统等价为完全可控型线性化模型,然后设计了滑模变结构控制器,并利用模糊控制器实现了滑模趋近律的参数自整定,设计方法简单可行。仿真结果表明,所设计的模糊滑模控制器能够快速准确地跟踪设定航向,并对参数摄动和外界风浪干扰具有很强的鲁棒性,同时消除了系统的抖振现象,优于传统的滑模控制。

Abstract：

According to the nonlinear model of ship autopilot system and using the feedback linearization procedure of differential geometry,an equivalent,fully controllable and linear model was derived via a homomorphism transformation and a fuzzy reaching law sliding mode controller was designed.The simulation results show that the controller designed here,which is superior to traditional sliding mode control,can track a desired course fast and accurately.It also exhibits strong robustness peculiarity to system uncertainties and avoiding chatting phenomenon.     

装甲装备月份维修计划优化制订方法研究

分析装甲装备月份维修计划的制订目前存在的问题,通过研究任务与装甲装备月份维修计划之间的相关关系,提出了根据任务的强度确定维修时机为优化目标的维修计划优化模型,统筹考虑维修资源、规章制度等因素。经LINGO软件仿真验证,结果显示该模型能够极大化装备的使用效益,实现科学化、精确化的送修,以及对装备的集约化管理。

Abstract：

The problems were analyzed that lay in the formulation of the armored equipment month maintenance plan. Based on researches about the relationship between the mission and the month maintenance plan, a maintenance plan optimization formulation model was brought forward. The model took factors such as maintenance resources, rules and regulations into overall consideration, and selected maintenance opportunity based on the strength of the mission as optimization goal. The model was validated by LINGO simulation. The result shows that the model can not only maximize the use efficiency, but also realize the scientific and precise delivery and the intensive management of the equipment which needs preventive maintenance.     

高速磁浮曲线地段简支轨道梁墩体系动力响应仿真

应用桥梁动力学、车辆动力学和电磁相互作用原理建立了高速常导磁浮交通车-梁-墩体系动力分析模型,利用数值积分求解了大规模非线性耦合动力方程.在此基础上结合具体线路条件进行了车线耦合动力学检算,得到了曲线地段车辆及梁墩体系动力响应基本规律.该部分的研究为制订合理的高速磁浮线路设计标准提供了理论依据.     

一种共前缀码的测试数据压缩方案

提出了一种新的基于游程编码的测试数据压缩/解压缩的算法:共前缀码编码(SPCS),它在传统游程使用较短的代码字来代替较长的游程的基础上,进一步探讨游程之间的相关性,使用一位来代替具有与前一游程相同前缀的后一游程的前缀,使需要多位才能表示的代码字的前缀用-位就可以表示,进一步提高了压缩率.相比类似的编码测试数据压缩方案,具有压缩率高、解压控制过程容易实现的突出特点.理论分析和对ISCAS-85和ISCAS-89部分标准电路硬故障集的实验结果证明了本方案的有效性.     

不确定时滞系统的区间时滞相关鲁棒镇定

研究了时间滞后满足区间变化的线性连续系统鲁棒镇定问题。采用Lyapunov-Krasovskii稳定性分析方法,给出了区间时滞依赖系统的状态反馈设计稳定解。进一步研究参数化不确定性情况下,区间时滞依赖系统的鲁棒稳定性判据和鲁棒状态反馈控制器设计方法。最后,通过仿真算例比较,验证了此方法的有效性。     

UCAV编队协同对地攻击决策系统研究

针对UCAV编队对地攻击系统,提出了有人机UCAV联合编队协同对地攻击的概念,分析了有人机UCAV编队对地攻击的体系框架,提出了编队对地攻击的系统结构及其功能划分,给出了对地攻击的作战流程.基于UCAV编队对地攻击决策的复杂性,决策信息的分布性以及决策过程的层次性,提出了UCAV编队时地决策知识的表达和推理方法.