Research on consistency measurement and weight estimation approach of hybrid uncertain comparison matrix

The consistency measurement and weight estimation approach of the hybrid uncertain comparison matrix in the analytic hierarchy process （AHP） are studied. First, the decision-making satisfaction membership function is defined based on the decision making＇s allowable error. Then, the weight model based on the maximal satisfactory consistency idea is suggested, and the consistency index is put forward. Moreover, the weight distributing value model is developed to solve the decision making misleading problem since the multioptimization solutions in the former model. Finally, the weights are ranked based on the possibility degree approach to obtain the ultimate order.     

Observer-based H∞ control over packet dropping networks

A new controller design problem of networked control systems with packet dropping is proposed. Depending on the place that the observer is put in the system, the network control systems with packet dropping are modeled as stochastic systems with the random variables satisfying the Bernoulli random binary distribution. The observer-based controller is designed to stabilize the networked system in the sense of mean square, and the prescribed H∞ disturbance attenuation level is achieved. The controller design problem is formulated as the feasibility of the convex optimization problem, which can be solved by a linear matrix inequality (LMI) approach. Numerical examples illustrate the effectiveness of the proposed methods.     

Robust model predictive control of continuous uncertain systems*

The authors concern robust model predictive control for linear continuous systems with polytopic uncertainties and input constraints. At each sampling time, a piecewise constant control sequence is obtained by solving a set of linear matrix inequalities. The sufficient conditions on the existence of the model predictive control are given, and the robust stability of the closed-loop systems is guaranteed. A simulation example illustrates the efficiency of the proposed method.     

二次D稳定约束下不确定T-S模糊系统的L∞鲁棒可靠控制

针对一类受持续有界扰动的T-S不确定模糊系统,提出了考虑执行器故障的鲁棒可靠控制器设计方法。引入基于L_∞范数理论的鲁棒性能指标及二次D稳定的概念,给出了鲁棒可靠控制器存在的充分条件。通过求解线性矩阵不等式完成可靠控制器的设计,从而使系统即使在发生执行器故障的情况下仍能满足给定的L_∞性能指标,并且闭环系统二次D稳定。仿真实例表明了本方法的有效性。     

冲击噪声背景下宽频段信号三维参数的估计

提出了一种基于协变异矩阵的宽频段信号频率和二维到达角联合估计的算法。在冲击噪声环境下,该算法能精确地估计宽频段信号的三维参数,无需多维谱峰搜索和参数配对过程。另外,利用L型阵列的分维特点和ESPRIT算法进一步处理,成功地实现了具有频率兼并现象的宽频段信号的三维参数估计。计算机仿真结果验证了算法的有效性。     

广义交叉乘积累加码

为设计具有线性编、译码复杂度及逼近香农限性能的信道编码结构,在并行级联的单奇偶校验码之间引入交叉结构以构成外码,以累加器为内码,提出了一种新的串行级联编码--广义交叉乘积累加码。以外信息转移图为工具对广义交叉乘积累加码进行设计,并给出一个广义交叉乘积累加码的设计示例。分析及仿真结果表明,该示例具有线性编、译码复杂度,其收敛门限距香农限仅有约0.32 dB的距离。     

X波段瞬态极化雷达射频前端关键技术研究

瞬态极化新体制雷达,通过单脉冲获得瞬时极化散射矩阵来提取目标特征信息,提高了雷达系统在复杂电磁环境中的探测、抗干扰和反隐身等方面能力。基于该雷达工作原理,提出“同时正交双极化”的射频前端设计方案,完成了国内首部瞬态极化雷达试验系统射频前端的研发。采用正交双通道和幅相一致性技术保证了雷达实现瞬态极化的功能,采用滤波技术保证了射频系统的频谱纯度;采用低噪声放大技术有效降低了接收机噪声系数;采用直接频率综合技术提高了射频系统频率稳定度和相参性能;结构集成一体化设计保证了射频收发前端的电磁兼容性能和便携性。射频前端测试结果均优于指标要求,并支持试验系统初步解决了目标极化散射特征提取与识别领域的基础性和共性难题。     

Calibration method of phase distortions for cross polarization channel of instantaneous polarization radar system

A novel poladmetric calibration method for new target property measurement radar system is presented.Its application in the real radar system is also discussed.The analysis indicates that instantaneous polarization radar (IPR) has inherent cross-polarization measurement error.The proposed method can effectively eliminate this error,and thus enhance the polarization scattering matrix (PSM) measurement precision.The phase error caused by digital receiver's direct iF sampling and mixing of two orthogonal polarization channels can be removed.Consequently,the inherent error of target polarization scattering measurement of the instantaneous polarization radar system is well revised.It has good reference value for further plcarimetric calibration and high practical application prospect.     

对称机动飞行时飞行员人体动态体表压力分布研究

论述了飞行员人体动态体表压力分布对于飞行过载动感仿真的重要性。给出坐姿人体体表压力模式及其等效压力分析方法。在对称机动飞行情形下,建立了飞行员人体动力学方程,该方程考虑了歼击机飞行员实际坐姿。导出了动态体表压力公式,动态体表压力与飞行员人体加速度之间的惯性传递矩阵。给出与动态体表压力相关的歼击机飞行员人体参数计算方法。以某飞机眼镜蛇机动为例,通过数值求解,得到该机动飞行时飞行员人体动态体表压力分布。研究结果可用于指导过载椅设计。     

基于Simulink的广义执行机构仿真模型库建模

为了提高方案生成后仿真模型的建模效率,建立了基于Simulink的广义执行机构仿真模型库。该模型库将广义执行机构分为执行机构和驱动元件两类,分别建立了支持广义执行机构仿真的执行机构库和以驱动输入分类的驱动元件模型。其中执行机构库使用屏蔽实现了模型接口的封装,同时将每个模型的基本参数定义为变量来表示。设计者可通过直接搜索调用方案解对应的仿真原型或分解和手工合并相关模型文件来快速构建仿真模型。以某船载装置移动机构和惯性振动筛机构的方案设计为例说明了仿真模型库的有效性。