侧风状况下轿车气动特性的仿真与实验研究

以获得适合计算侧风气动特性的湍流模型为目的,应用计算流体动力学方法对比了标准k模型、RNG k模型、Realizable k模型以及SST模型对不同横摆角状态下轿车气动特性仿真结果的影响。结果表明,当0时,采用Realizable k湍流模型仿真得出的阻力系数与实验结果最为吻合,误差仅为1.53%,侧力系数的仿真结果与理论分析更为吻合;当3～1 5时,采用Realizable k湍流模型仿真得出的阻力系数与实验结果相比误差最大为0.96%,侧力系数的仿真结果与实验结果趋势一致,误差最大也仅为4.9%。总之,Realizable k湍流模型能够很好的模拟侧风状态下车辆的气动特性,仿真结果为进一步分析车辆的侧风稳定性提供了参考数据。     

基于DCS的发射分集MIMO雷达参数估计

针对目标在多角度观测下的散射系数估计问题,研究了基于分布式压缩感知（distributed compressed sensing, DCS）的发射分集多输入多输出（multiple-input multiple-output, MIMO）雷达参数估计方法。在分析发射分集MIMO雷达信号模型的基础上,构建了其联合稀疏表示模型;在分析正交匹配追踪（orthogonal matching pursuit, OMP）算法实现结构的基础上,提出了一种新的基于迭代式正交匹配追踪的DCS算法。仿真结果表明该方法的估计精度高于DCS SOMP和幅度相位估计+Capon的算法,重构概率也高于DCS-SOMP算法。     

Multi-target localization for bistatic MIMO radar in the presence of unknown mutual coupling

A decoupling-estimation signal parameters via rotarional invariance technique(ESPRIT) method is presented for multi-target localization with unknown mutual coupling in bistatic multiple-input multiple-output(MIMO) radar.Two steps are carried out in this method.The decoupling operation between angle and mutual coupling estimates is realized by choosing the auxiliary elements on both sides of the transmit and receive uniform linear arrays(ULAs).Then the ESPRIT method is resilient against the unknown mutual coupling matrix(MCM) and can be directly utilized to estimate the direction of departure(DOD) and the direction of arrival(DOA).Moreover,the mutual coupling coefficient is estimated by finding the solution of the linear constrained optimization problem.The proposed method allows an efficient DOD and DOA estimates with automatic pairing.Simulation results are presented to verify the effectiveness of the proposed method.     

非线性多智能体系统分布式鲁棒输出调节

为解决具有一般非线性形式和不确定参数的多智能体系统的协调控制问题,设计了非线性分布式反馈控制器,使得多智能体系统鲁棒渐近跟踪参考信号或者鲁棒渐近抑制干扰。在所考虑的多智能体系统中,将动态领导者或者环境干扰看作是产生参考信号或者干扰信号的外部系统。最后,给出一个仿真算例,验证所得结果的有效性。     

基于正则信道求逆预编码的MIMO功率分配方案研究

提出一种多用户MIMO系统中基于正则信道求逆预编码并具有QoS保障的功率分配方案:结合信道状态信息和用户QoS需求,分析得出约束条件的可行性判断依据;利用连续几何规划算法将非凸优化问题近似为凸优化问题,并辅以内点法求解最优功率分配方案;最终综合得出一套基于滑动窗口机制的功率分配框架。仿真结果表明,与现有算法相比,该方案能在有效保障用户最小速率和时延需求的基础上,显著提高系统可达速率。     

有源电力滤波器直流侧电压控制系统的仿真

针对有源电力滤波器的特点,提出一种用MATLAB/Simulink元件库中的电力电子器件建立闭环控制系统的仿真模型,用特有的S函数对改进的ip-iq算法编程实现。仿真分析了投入APF前后系统建立过程各个变量的状态变化,针对其结果进行了定性分析研究,分析影响APF投入及其直流侧电压控制的各种因素。仿真分析表明,系统仿真模型有效地模拟了系统启动过程中,补偿电流指令及直流侧电压的过渡过程,对研究和应用数字化控制技术的有源电力滤波系统具有重要指导意义。     

人工神经网络在汽车轮胎侧偏特性研究中的应用

引入人工神经网络理论中应用广泛的多层前向ＢＰ网络模型,进行汽车动力学仿真中轮胎侧偏特性的研究,得到轮胎侧偏特性的人工神经网络模型,并以实例验证这种建模方法的准确性和实用性。     

MIMO雷达反向投影成像算法

针对多输入多输出(multiple-input multiple-output, MIMO)雷达的多收发固定阵列结构,在标准反向投影(back projection, BP)成像算法基础上,提出了一种修正BP成像算法。该算法首先对MIMO雷达距离压缩回波数据进行时延曲线校正处理,而后沿方位向直接相干叠加各路回波处理数据,从而无需距离插值即可实现方位聚焦。与标准BP算法相比,修正BP算法大大降低了运算量,同时也克服了现有快速BP算法大都没有考虑距离插值运算的缺陷。MIMO雷达外场实测数据处理表明：与标准BP算法相比,修正BP算法有效节省了运算时间,并保持了雷达成像质量。     

Robust H∞ control for neutral stochastic uncertain systems with time-varying delay

The problem of robust H∞ control for uncertain neutral stochastic systems with time-varying delay is discussed. The parameter uncertaintie is assumed to be time varying norm-bounded. First, the stochastic robust stabilization of the stochastic system without disturbance input is investigated by nonlinear matrix inequality method. Then, a full-order stochastic dynamic output feedback controller is designed by solving a bilinear matrix inequality (BMI), which ensures a prescribed stochastic robust H∞ performance level for the resulting closed loop system with nonzero disturbance input and for all admissible uncertainties. An illustrative example is provided to show the feasibility of the controller and the potential of the proposed technique.     

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.