准正交空时分组码的自适应设计

为了能在满足空时分组码完全分集的同时尽可能降低译码复杂度,提出了准正交空时分组码的自适应设计方案. 在准正交空时分组码的编码结构上添加自适应系数,根据当前信道状态信息计算自适应系数的具体数值. 设计的目的是保证传输的数据符号之间相互正交,彼此没有干扰,从而实现完全分集,并能采用复杂度低的单符号译码方法. 仿真结果表明,准正交空时分组码自适应方案的误码率性能要明显好于采用星座旋转的准正交空时分组码方案,只需要采用有限反馈的方法就能实现近似理想反馈的误码率性能.      

煤矿工作面无线全覆盖通信系统设计

根据煤矿工作面无线通信的需求,分析了现有工作面有线通信和无线通信技术的优缺点,提出了一种基于无线网状网和ZigBee技术的煤矿工作面无线全覆盖通信系统设计方案,并介绍了综合基站和WiFi网关的设计。测试结果表明,该系统能够满足工作面数据、语音、视频等不同信息的无线传输需求,实现了工作面无线信号的全覆盖。     

机械电器产品检验抽样方法探讨

根据机电产品生产特点,对稳定生产状态下的生产条件进行细分,提出不同生产条件下的生产质量验收抽样方法。     

注塑整圆内侧倒扣塑料件的分步抽芯法

针对具有整圆内侧倒扣特征的塑料件,设计了一种新型的注塑模具分步抽芯机构,并使用Pro/Mechanism软件对该机构进行了运动模拟仿真,证明该分步抽芯机构的设计是切实可行的。     

某型装甲车制动器热-应力-磨损耦合仿真分析

为提高鼓式制动器在热-应力耦合影响下磨损计算的准确性,考虑实际制动过程中温度升高对制动器性能的影响,通过增加温度与磨损率的变化关系修正传统Archard磨损模型,对某型装甲车鼓式制动器进行仿真计算.分析结果表明,在热-应力有限元迭代求解过程中,采用完全耦合法持续更新制动器磨损面的几何形状可以不断地修正热-应力的计算结果,因此能更真实地描述制动过程中热-应力-磨损的复杂耦合现象.仿真得到制动器在4种典型工况下的磨损规律,为制动器的优化设计提供依据.     

基于多特征融合与ResNet的海面溢油区识别研究

近年来,合成孔径雷达（SAR）在改善溢油检测方面得到了广泛应用。然而,由于其特殊的成像机理,乘性相干斑噪声和其他物理现象引起的暗斑一直影响着溢油检测的精度。单独使用一种特征很难对图像上的油膜和类油膜现象进行区分,针对这一问题提出了利用多特征融合结合深度残差网络（ResNet）的方式来区分全极化图像上的油膜和类油膜现象。实验中将C波段的三种极化特征：极化散射熵（Entropy）、平均散射角（Alpha）和单次散射特征值相对差异度（SERD）组合在一起,形成一个优化特征子集,在确定的三种极化特征对应的特征图上选取多个感兴趣区域作为ResNet网络的训练集和测试集。该实验所用训练集由3 600个原油样本、3 600个生物油样本和3 600个乳化油样本（共计10 800个）组合而成。测试集由600个原油样本、600个生物油样本和600个乳化油样本（共计1 800个）组合而成,最终得到97.56%的分类精度。用同样的实验数据采用同是深度学习的VGG和AlexNet分类算法进行油膜和类油膜的分类,并与ResNet算法分类结果进行对比分析。为了减弱过拟合现象以及获得更可靠的实验结果,分别进行了[K]-交叉验证和ROC曲线实验。结果表明所提出的算法是有效的。     

Fault estimation for aero‐engine LPV systems based on LFT

In this paper, a fault estimator with linear fractional transformation (LFT) parameter dependency is designed for the linear parameter‐varying (LPV) system of the aero‐engine with both sensor and actuator faults under disturbances. After an aero‐engine affine parameter‐dependent LPV model is derived by the linear fitting method and matrix pseudo‐inverse method, the LPV model with disturbances and fault signals is transformed into a LFT structure. Based on the full block S‐procedure, the sufficient condition for the existence of the fault estimator is proposed, which can lead to less conservative results. Then the fault estimator design algorithm which can adjust to the current system dynamic adaptively is presented. Finally, a fault estimator is designed for a turbofan aero‐engine under multiple types of faults and disturbances to demonstrate the effectiveness of the proposed method.     

Investigation on full vehicle height control algorithm using feedback linearization method

Aiming to improve the control accuracy of the vehicle height for the air suspension system, deeply analyzing the processes of variable mass gas thermodynamics and vehicle dynamics, a nonlinear height control model of the air suspension vehicle was built. To deal with the nonlinear characteristic existing in the lifting and lowering processes, the nonlinear model of vehicle height control was linearized by using a feedback linearization method. Then, based on the linear full vehicle model, the sliding model controller was designed to achieve the control variables. Finally, the nonlinear control algorithm in the original coordinates can be achieved by the inverse transformation of coordinates. To validate the accuracy and effectiveness of the sliding mode controller, the height control processes were simulated in Matlab, i.e., the lifting and lowering processes of the air suspension vehicle were taken when vehicle was in stationary and driving at a constant speed. The simulation results show that, compared to other controllers, the designed sliding model controller based on the feedback linearization can effectively solve the "overshoot" problem, existing in the height control process, and force the vehicle height to reach the desired value, so as to greatly improve the speed and accuracy of the height control process. Besides, the sliding mode controller can well regulate the roll and pitch motions of the vehicle body, thereby improving the vehicle''s ride comfort.     

深部巷道方钢约束混凝土拱架力学性能及影响因素研究

对全尺寸直腿半圆形拱架进行了室内试验和数值分析,室内试验表明:拱架的变形破坏呈现"拱腿内挤,拱顶外凸"的特点,拱腿和拱顶部位的钢材达到塑性状态,极限承载力Fe=1 228kN.针对充填C30~C80强度混凝土以及壁厚4~12 mm的SQCC拱架的数值分析表明:SQCC150-8-C30拱架的极限承载力为1 217kN,拱架极限承载力差异率为0.89%,拱架变形破坏特征和钢材的应力应变状态都和室内试验结果吻合.通过数值分析可见钢管壁厚比核心混凝土强度对拱架极限承载力的影响更为显著;建议壁厚8mm,C30或C40核心混凝土强度的SQCC拱架较为适用.     

Research and Application of Dynamic Equation for Full Frontal Impact

Full frontal impact theory needs researching and exploring to satisfy the primary safety design of occupant restraint system,avoiding the increasingly "engineering"trend in order to develop and design safety vehicle. After occupant restraint system is simulated by using linear elastic stiffness k,the occupant-vehicle frontal rigid barrier impact model is established. Dynamic equation of dummy chest coupling vehicle is built for full frontal impact based on ordinary vehicle deceleration by Hooke law,and the equation is solved by comparing coefficient and satisfying boundary qualifications. While relative vehicle characteristic parameters are kept unchanging,the actual vehicle deceleration is fitted to the simplified equivalent square wave( ESW),tipped equivalent square wave( TESW) and equivalent dual trapezoids wave( EDTW). Phase angle  and amplitude A of dynamic equations based on ESW,TESW and EDTW are calculated and deduced. The results show that: the dynamic equation of dummy chest coupling vehicle can be well utilized to instruct the primary safety design of full frontal impact for objective vehicle to satisfy chest deceleration demands and the equation based on TESW is best for this design.