电子干扰飞机对抗警戒雷达组网系统的效果评估

在复杂的电磁环境下,如何有效地分析和评估远距离支援干扰对抗地面防空雷达网的效果具有重要的意义。分析了电子干扰飞机的运动给干扰效果造成的影响,以噪声压制式干扰效果评估为例,针对警戒雷达及其组网系统,在"有效干扰区"、"暴露区"等传统评估指标的基础上,提出增加"干扰过渡区"作为评估指标,研究了相应的评估方法,并给出了干扰效果的定量评估结果。     

基于循环累积量的星形QAM载波盲估计

针对通信对抗和正交幅度调制(QAM)信号解调的实际应用,提出一种利用特定高阶循环累积量估计星形QAM载波的方法。由于高阶循环累积量能有效抑制平稳噪声和非平稳高斯噪声,通过理论分析可证明在上述噪声背景下,星形8、16 QAM信号的特定四阶循环累积量仅在载波位置处存在,因此可以通过检测此循环频率实现载波的估计。该算法可推广到更高阶星形QAM信号。仿真实验验证了该算法的有效性。     

基于MQNM的双基地雷达目标定位改进算法

针对求解双基地雷达目标定位问题常用的Gauss-Newton法自身固有的缺点,如收敛精度和收敛速度依赖于迭代初值与真实值的接近程度和函数的非线性程度,进一步考虑了目标函数Hessian阵的二阶信息,结合MQNM法(修正拟牛顿法)提出了一种双基地雷达目标定位问题的优化改进算法。计算机仿真结果表明了该算法的可行性和有效性。     

Gate-to-Gate模式下航班到达的综合调度

Gate-to-Gate是空中交通管理的未来趋势之一,研究了Gate-to-Gate模式下的航班到达问题,对航班到达的空中降落与地面滑行进行综合调度,建立了地空综合调度的简化数学模型,实现了航班到达从区调阶段到航站楼的关键点路径规划和时间安排,并对北京终端区及首都机场地面滑行过程进行了算例分析。针对实际应用规模大、求解时间长的问题,利用模型的特殊性制定了先松弛后固定分支求解的两步法求解算法,实现了在5分钟内能求得相对误差小于5.3%的近优解。     

基于时变偏差分离估计的杂波下机动目标跟踪

在杂波环境机动目标跟踪问题中,波门位置和范围的确定是关键技术之一。在分析了时变偏差分离估计算法的有偏差的状态估计协方差基础上,提出了基于时变偏差分离估计(separate bias estimation, SBE)和概率数据关联(probabilistic data association, PDA)的新算法,利用了偏差估计和有偏差的状态估计协方差来确定波门位置和范围,并结合PDA处理多个回波的能力,实现杂波环境下机动目标的跟踪。通过仿真实验,说明了新算法的优势和有效性。     

毫米波FPA成像系统馈源天线研究

毫米波焦平面阵列（focal plane array,FPA）成像系统中,馈源天线的排列密度是决定系统空间采样率的主要因素。提出了一种新型结构的介质棒天线,相对于其他馈源天线,它具有宽频带、低副瓣、低互耦和低交叉极化,通过改变长度而不是横截面来改变天线增益等优点,易于排成紧密的馈源阵列,以更低的溢出损耗实现对透镜或反射面天线的有效照射。通过详细的理论分析、仿真和优化设计,研制了介质棒天线及其阵列并将其应用于毫米波FPA成像系统中。该系统可用于探测人体隐匿物品,成像效果较好。     

Target location with signal fitting and sub-aperture tracking for airborne multi-channel radar

The location of a moving target based on signal fitting and sub-aperture tracking from an airborne multi-channel radar is dealt with. The proposed approach is applied in two steps: first, the ambiguous slant-range velocity is derived with a modified single-snapshot multiple direction of arrival estimation method, and second, the unambiguous slant-range velocity is found using a track-based criterion. The prominent advantage of the proposed approach is that the unambiguous slant-range velocity can be very large. Besides, the first stage is carried out at the determinate range-Doppler test cell by azimuth searching for fitting best to the moving target signal, therefore, the location performance would not be sacrificed in order to suppress clutter and/or interference. The effectiveness and efficiency of the proposed method are validated with a set of airborne experimental data.     

正负靶心灰靶决策模型

对灰靶决策模型进行了进一步的拓展研究.定义理想最优及理想最劣方案分别为灰靶的正负靶心,在综合考虑方案与正负靶心的距离,将靶心距作为向量在空间分析的基础上定义了综合靶心距.由各方案靶心距大小及指标权重的不确定性分析的基础上构建目标规划,并由此确定指标权重.由此建立了正负靶心灰靶决策模型.最后以实例说明了所提出的灰靶决策模型的合理性及算法的有效性.     

Modeling for UAV resource scheduling under mission synchronization

Unmanned aerial vehicle (UAV) resource scheduling means to allocate and aggregate the available UAV resources depending on the mission requirements and the battlefield situation assessment. In previous studies, the models cannot reflect the mission synchronization; the targets are treated respectively,which results in the large scale of the problem and high computational complexity. To overcome these disadvantages, a model for UAV resource scheduling under mission synchronization is proposed, which is based on single-objective non-linear integer programming. And several cooperative teams are aggregated for the target clusters from the available resources. The evaluation indices of weapon allocation are referenced in establishing the objective function and the constraints for the issue. The scales of the target clusters are considered as the constraints for the scales of the cooperative teams to make them match in scale. The functions of the intersection between the "mission time-window" and the UAV "arrival time-window" are introduced into the objective function and the constraints in order to describe the mission synchronization effectively. The results demonstrate that the proposed expanded model can meet the requirement of mission synchronization, guide the aggregation of cooperative teams for the target clusters and control the scale of the problem effectively.     

飞机结冰包线保护对开环飞行性能影响与仿真

在所有的飞机失事事故中,由于飞机结冰造成的灾难是很重要的因素之一。为了解决飞机结冰后造成的飞机失速迎角减小以及飞行包线萎缩等安全隐患,通过引入结冰参数等,采用一种简化的飞机结冰模型的方法来仿真。仿真计算各种输入或者扰动下,结冰飞机纵向各项性能响应。通过在线计算结冰失速迎角,建立开环状态下飞机包线保护系统,实时反馈失速迎角告警信息以提醒飞行员操作,从而保证飞机飞行的安全。仿真计算表明,该方法行之有效,而且概念清晰,计算简便,可以在实验条件不足的情况下,为仿真研究提供一种良好的方法。

Abstract：

In-flight icing is one of the most important factors for all of the aircraft accident.A brief method was utilized to simulate the aeroplane iced in order to solve the problem which was caused by ice,such as low stall of angle of attack and flight envelope atrophy.All the longitudinal dynamic of aircraft could be got in different input.Ice aircraft envelope protection could provide the pilot with enough time to avoid icing related accidents by calculating the stall limits of angle of attack online.The result of simulation can show that the system is working effectively,furthermore its method is simple and concept is obvious.It provides a good way for simulation research,especially in the condition of experiment lacking.