基于遗传算法的航向测量误差分析

提出了一种基于遗传算法的高精度航向测量误差分析的方法,测量模型由2台全站仪组成.通过最佳保留策略和带约束条件的遗传算子,保证该算法具有全局搜索能力.分析结果表明,遗传算法的搜索空间仅为整个搜索空间的0.03%,该模型在现有码头条件下航向测量的精度可达到4″,满足对舰船导航设备高精度航向标校的要求.     

SINS/DR组合导航系统可观测性研究

对SINS/DR组合导航系统的误差方程进行了介绍。将陀螺漂移、加速度计零偏和里程仪刻度系数误差扩展为卡尔曼滤波器的状态,建立了19维状态的组合导航滤波模型。采用分段线性定常系统(PWCS)分析了载车在各个不同运动特性下SINS/DR组合导航系统的可观测矩阵;利用奇异值分解(SVD)分析法定量地分析了SINS/DR导航系统的可观测度。通过系统仿真预测了位置误差、姿态误差和速度误差的滤波效果,仿真结果表明,位置误差、姿态误差和速度误差的估计效果较好。     

Adaptive phasefield modelling of crack propagation in orthotropic functionally graded materials

In this work, we extend the recently proposed adaptive phase field method to model fracture in orthotropic functionally graded materials (FGMs). A recovery type error indicator combined with quadtree decomposition is employed for adaptive mesh refinement. The proposed approach is capable of capturing the fracture process with a localized mesh refinement that provides notable gains in computational efficiency. The implementation is validated against experimental data and other nu-merical experiments on orthotropic materials with different material orientations. The results reveal an increase in the stiffness and the maximum force with increasing material orientation angle. The study is then extended to the analysis of orthotropic FGMs. It is observed that, if the gradation in fracture properties is neglected, the material gradient plays a secondary role, with the fracture behaviour being dominated by the orthotropy of the material. However, when the toughness increases along the crack propagation path, a substantial gain in fracture resistance is observed.     

Cooperative interception with fast multiple model adaptive estimation

For the case that two pursuers intercept an evasive target, the cooperative strategies and state estimation methods taken by pursuers can seriously affect the guidance accuracy for the target, which performs a bang For the case that two pursuers intercept an evasive target, the cooperative strategies and state estimation methods taken by pursuers can seriously affect the guidance accuracy for the target, which performs a bang-bang evasive maneuver with a random switching time. Combined Fast multiple model adaptive estimation (Fast MMAE) algorithm, the cooperative guidance law takes detection configuration affecting the accuracy of interception into consideration. Introduced the detection error model related to the line-of-sight (LOS) separation angle of two interceptors, an optimal cooperative guidance law solving the optimization problem is designed to modulate the LOS separation angle to reduce the estimation error and improve the interception performance. Due to the uncertainty of the target bang-bang maneuver switching time and the effective fitting of its multi-modal motion, Fast MMAE is introduced to identify its maneuver switching time and estimate the acceleration of the target to track and intercept the target accurately. The designed cooperative optimal guidance law with Fast MMAE has better estimation ability and interception performance than the traditional guidance law and estimation method via Monte Carlo simulation.     

向量巨型机高效程序设计技术

本文着重研究适应向量巨型机体系结构的高效程序设计技术。围绕减少指令流水线阻塞,提高多功能部件并行度,数据调度与局部化技术三个方面进行了深入的讨论,给出了一系列设计高效程序的方法和技巧。     

基于车载GPS定位的固定目标坐标测量误差分析

通过分析地面移动侦察系统对固定目标进行一次坐标测量时的测量过程,建立了固定目标坐标测量模型。通过对测量过程中误差传递规律的分析,导出了目标坐标测量误差的分布规律。根据坐标测量误差中各组成成分的大小,将测量误差分布规律近似成正态分布,并给出了分布参数的简化计算方法。仿真结果证实了误差分布规律近似及参数计算简化的可行性。     

寻的制导控制系统设计方法探讨

对使用寻的体制探测目标的防空导弹制导控制系统设计方法进行了分析、探讨.设计中主要考虑了天线罩折射误差及去耦系数、有效导航比、稳定回路时间常数、气动力时间常数和遮挡效应的影响;对于低空制导控制系统主要考虑了多路径(镜像干扰)的影响,对布鲁斯特角效应抑制多路径(镜像干扰)的影响进行了分析.     

武装直升机无控武器射击误差源分析

探讨了影响武装直升机无控武器对地射击准确度的因素 ,建立了武装直升机对地射击瞄准方程 ,定量分析了主要误差源对射击准确度的影响 ,得出了必须修正直升机迎角、旋翼下洗气流和平均风对射击准确度影响的结论     

陀螺随机漂移误差模型建模方法研究

论述了自60年代以来的几种主要陀螺仪漂移误差模型建模的方法,介绍了各种方法的特点及建模公式,有助于惯导系统中陀螺漂移误差模型的建立．     

外槽轮机构分度精度分析与设计

分析了外槽轮机构主要零部件的设计精度对槽轮分度精度的影响 ,结果表明主动件长度和滚子与轮槽之间的间隙对分度精度影响最大。用概率与数理统计的方法导出了精度设计公式并给出一个计算实例