一种单轴旋转捷联惯导系统高精度快速对准方法

在晃动条件下,需要延长粗对准时间来提高粗对准精度。否则,无法把方位误差控制在小角度范围内,从而导致后续的精对准无法快速收敛。针对这个问题,提出了一种利用逆向导航技术的单轴旋转捷联惯导系统高精度快速对准方法,最大限度地延长粗对准时间,并把采样数据存储下来,进行逆向精对准。这种算法充分地利用了对准数据,在固定对准时间内极大程度的提高了对准精度。试验证明,这种算法计算量小,算法简单,能实现单轴旋转捷联惯导系统高精度快速对准,且对准精度高,具有一定的工程应用价值。     

采用组合优化策略求解导管桨参数优化设计问题

建立了新的导管桨优化设计模型。该模型采用试验设计方法(DOE,design of experiment)在设计空间中均匀采样,捕捉整个设计空间中最有效的设计区域,进而用梯度优化算法在有效设计区域中进行优化设计。经计算实例证明:该算法可以辨识各因子对设计目标的影响系数,从而减少导管桨约束优化问题的计算时间,更有效地解决复杂的非线性优化问题。     

基于改进Morison公式的海上漂浮软管波浪载荷计算

针对海上漂浮软管波浪载荷计算,分析了软管在海上的形态和受力特点,建立了海上漂浮软管力学分析模型,指出直接运用现有Morison方程计算漂浮软管波浪载荷存在的不足,并根据基本原理提出了改进Morison方程。对海上软质管线处于一定海况,分别运用改进Morison方程与现有Morison方程计算海上波浪载荷,并运用ANSYS软件建立软管模型,结果表明现有Morison方程不适用于计算海上漂浮软管波浪载荷,载荷计算结果偏高约15%,从而验证了改进Morison方程的精确性,有利于准确分析波浪载荷对海上漂浮软管的作用情况。     

基于混合高斯概率密度的加权打分方法

针对当前评比打分方法不能有效反映选手真实情况的问题,提出了一种基于混合高斯概率密度的加权打分方法。该方法的重点在于引入混合高斯分布来确定专家评分的权重。首先利用EM算法确定混合高斯分布模型参数,然后通过区间划分得到每个区间上的概率,再将专家打分映射到混合高斯概率密度函数区间上得到对应的权重,最后经加权求和得到选手的最终成绩。通过实例证明了该方法的合理性和公正性。     

大学自习教室优化设置研究

针对目前大学自习教室资源浪费普遍存在的现象,将学生上自习与否视为独立同分布随机变量,从自习教室的管理与维护成本、电费成本以及学生的满意度3个方面出发,建立了双目标随机规划模型,并在模型基础上提出了大学自习教室设置的一般方法。通过实例分析,对模型的正确性和有效性进行了论证。结果表明:在各种情况下,该模型都能很好地解决自习教室设置这一问题,并且能在学生满意度较高的条件下,节约能源13%以上。该模型可以有效地对自习教室进行优化设置,不仅提高了资源利用水平,而且节约了能源。     

基于可变增益的码跟踪环路优化设计

针对在突发直接序列扩频(DSSS)信号跟踪中,信号持续时间短,而传统延迟锁定环(DLL)存在入锁时间长的问题,提出一种可变增益码跟踪环路设计方法。介绍了DLL环路基本原理和环路结构,对环路优化进行了理论分析,最后采用可变增益设计方法,自适应的调整环路增益,达到锁定时间和跟踪精度的平衡。通过仿真分析,在相同跟踪精度上,与传统DLL环路相比,锁定时间大大缩短。     

Two novel critical shock models based on Markov renewal processes

In this paper, we investigate systems subject to random shocks that are classified into critical and noncritical categories, and develop two novel critical shock models. Classical extreme shock models and run shock models are special cases of our developed models. The system fails when the total number of critical shocks reaches a predetermined threshold, or when the system stays in an environment that induces critical shocks for a preset threshold time, corresponding to failure mechanisms of the developed two critical shock models respectively. Markov renewal processes are employed to capture the magnitude and interarrival time dependency of environment-induced shocks. Explicit formulas for systems under the two critical shock models are derived, including the reliability function, the mean time to failure and so on. Furthermore, the two critical shock models are extended to the random threshold case and the integrated case where formulas of the reliability indexes of the systems are provided. Finally, a case study of a lithium-ion battery system is conducted to illustrate the proposed models and the obtained results.     

Controllable combustion behaviors of the laser-controlled solid propellant

Microsatellites have been widely applied in the fields of communication,remote sensing,navigation and science exploration due to its characteristics of low cost,flexible launch mode and short development period.However,conventional solid-propellant have difficulties in starting and interrupting combustion because combustion is autonomously sustained after ignition.Herein,we proposed a new type of solid-propellant named laser-controlled solid propellant,which is sensitive to laser irradiation and can be started or interrupted by switching on/off the continuous wave laser.To demonstrate the feasibility and investigate the controllable combustion behaviors under different laser on/off conditions,the combus-tion parameters including burning rate,ignition delay time and platform pressure were tested using pressure sensor,high-speed camera and thermographic camera.The results showed that the increase of laser-on or laser-off duration both will lead to the decrease of propellant combustion performance during re-ignition and re-combustion process.This is mainly attributed to the laser attenuation caused by the accumulation of combustion residue and the change of chamber ambient temperature.Simultaneously,the multiple ignition tests revealed that the increased chamber ambient temperature after combustion can make up for the energy loss of laser attenuation and expansion of chamber cavity.However,the laser-controlled combustion performance of solid propellant displayed a decrease trend with the addi-tion of ignition times.Nevertheless,the results still exhibited good laser-controlled agility of laser-controlled solid propellant and manifested its inspiring potential in many aspects of space missions.     

应用语义关系自动构建情感词典

构建英文情感词典研究相对成熟,形成了丰富可靠的词典资源。而针对中文的研究时间短,中文情感分析词典资源较少。借鉴现有可靠的英文词典资源,提出了基于语义关系的情感词典自动构建算法,算法先从HowNet的概念中进行中文义原和词语抽取及语义分析,再利用HowNet概念中DEF中英文属性值,在英文情感词典SentWordNet中进行义原和词语情感值查询,最后根据词语和义原之间的语义关系进行词语的情感值计算。算法直接利用现有的英文情感词典,无须人工标注,生成的情感词典记录了词语的语义关系、情感极性值等多种信息,弥补了现有词典的不足。评测实验结果表明,根据算法实现的情感词典相比其他词典在准确率接近的情况下,召回率和F值最高,取得了较好的评测性能。     

鱼雷贮存战备完好率模型

为了评估鱼雷综合特性参数鱼雷贮存战备完好率,分析了国军标中基本模型,对照鱼雷寿命剖面,指出基本模型在具体鱼雷装备中应用存在的不足;通过对鱼雷寿命剖面中的基层级维修的深入分析,综合考虑贮存可靠度、故障检测率、鱼雷故障修复概率与备件满足率,给出了一个LRU故障、多个相同LRU故障以及多个不同LRU故障时的战备完好率模型。并通过计算验证了该模型的有效性。