基于凸优化理论的三维微分对策制导规律求解

针对三维微分对策制导律(DGL)求解问题,引入凸优化理论,将DGL求解归结到Hamilton系统的求解,设计了DGL求解算法,通过对代价函数梯度特征的凸分析,推导出对策系统鞍点存在的充要条件和求解方法,解决了以往通过对微分对策模型简化求解导致的模型不能客观反映作战过程的问题.     

面向反导预警作战的雷达交接班时机选择方法

针对反导预警作战过程中远程预警相控阵雷达(early-warning radar,EWR)和多功能地基相控阵雷达(ground-based radar,GBR)探测跟踪弹道导弹的交接班问题,提出了一种可行的雷达交接班时机选择方法.该方法通过卡尔曼滤波对弹道目标进行滤波定轨,基于目标瞬时运动状态估算目标剩余飞行距离,并依据GBR对目标的探测定位精度(geometrical dilution of precision,GDOP)进行接班时机优选,以支持反导预警作战雷达交接班决策.最后,通过一个实例验证了该方法的可行性和有效性.     

目标起伏特性对雷达威力性能的影响分析

介绍了典型雷达目标RCS起伏模型,阐述了起伏目标在实际中的应用,建立了目标损耗和雷达作用距离之间的关系,为不同目标的等效替代推算提供了理论依据.验证了雷达目标满足卡平方分布时发现概率和起伏因子之间的关系.并针对不同类型的起伏目标,建立了雷达探测距离和发现概率之间的关系,为雷达的威力检测和飞行目标的航线设计提供依据.     

基于多假设跟踪弹道导弹主动段跟踪算法

针对弹道导弹主动段防御中多枚弹道导弹同时跟踪问题,提出了基于多假设思想的主动段跟踪算法.重点阐述了该算法中假设生成、假设概率计算、假设约简以及假设剪枝等环节.从工程实用的角度出发,采用求解一个线性分配问题(LAP)方法得到M个最优假设,大大减少了假设数量,并运用N-scan回溯剪枝方法对假设进行剪枝,确定要输出的航迹,提高了算法的效率和实用性.仿真实验表明,该算法能够对主动段多枚弹道导弹目标准确关联跟踪.     

Adaptive sliding mode control of modular self-reconfigurable spacecraft with time-delay estimation

The reconstruction control of modular self-reconfigurable spacecraft (MSRS) is addressed using an adaptive sliding mode control (ASMC) scheme based on time-delay estimation (TDE) technology. In contrast to the ground, the base of the MSRS is floating when assembled in orbit, resulting in a strong dynamic coupling effect. A TED-based ASMC technique with exponential reaching law is designed to achieve high-precision coordinated control between the spacecraft base and the robotic arm. TDE technology is used by the controller to compensate for coupling terms and uncertainties, while ASMC can augment and improve TDE’s robustness. To suppress TDE errors and eliminate chattering, a new adaptive law is created to modify gain parameters online, ensuring quick dynamic response and high tracking accuracy. The Lyapunov approach shows that the tracking errors are uniformly ultimately bounded (UUB). Finally, the on-orbit assembly process of MSRS is simulated to validate the efficacy of the proposed control scheme. The simulation results show that the proposed control method can accurately complete the target module’s on-orbit assembly, with minimal perturbations to the spacecraft’s attitude. Meanwhile, it has a high level of robustness and can effectively eliminate chattering.     

One-bit splitting deceptive jamming against SAR

One-bit quantization is a promising technique due to its performance retention and complexity reduction in a deceptive jammer against synthetic aperture radar (SAR). In this paper, the 1-bit quantization technology is utilized to agilely generate split false targets in the SAR imagery once the radar signal is intercepted, which reduces the complexity of the jammer significantly with guaranteed focusing quality. A single-frequency threshold is used to decompose harmonics incurred by the 1-bit quantization, and its parameters are adjusted through different pulse repetition intervals to provide steerable modulations. In this way, the SAR signal is split into coupled false scatterers during the 1-bit interception. By further deploying amplitude, time-delay, and Doppler frequency modulations on the 1-bit intercepted signal, the split false targets are created. The proposed approach is compared with different deceptive jamming methods to show its validity in effectiveness and cost, and numerical experiments are also presented for verification.     

盲信道均衡的动量恒模算法

介绍了盲信道均衡恒模算法(CMA)的基本原理,对恒模算法的缺点进行了分析,通过修正恒模算法的迭代公式提出一种动量恒模算法(MCMA)。利用QPSK信号,采用计算机仿真的方法对动量恒模算法与恒模算法进行盲均衡性能比较,模拟结果显示,MCMA算法比CMA算法在收敛速率、降低稳态均方误差和符号间干扰具有明显的优势,有效地改进了信道均衡性能。     

含软判决引导的修正恒模盲均衡算法

在CMA算法基础上,提出了一种混合的修正恒模盲均衡算法MCMA SDD。新算法对CMA算法进行修正,同时引入软判决思想。理论分析和计算机模拟表明,该算法克服了CMA收敛速度慢、稳态误差大的缺点,同时可以纠正相位偏转。与CMA SDD算法相比,具有更快的收敛速度和更低的稳态均方误差。     

无人机虚拟维修训练系统及其HLA设计

以某型无人机虚拟维修训练系统的设计为实例,采用Creator对联邦实体建模,结合动态视景仿真软件Vega Prim e进行环境与目标的驱动,基于高层体系结构HLA对系统的分布式网络互联进行仿真设计,无人机虚拟维修训练系统有效地改善了目前无人机结合实装进行操作训练的局限性。     

基于GA的模糊PID控制在质量矩导弹系统上的应用

针对三轴稳定的质量矩导弹姿态控制系统,提出了一种基于遗传算法进行参数寻优的模糊PID控制方法。在建立姿控系统数学模型的基础上,首先设计了姿态控制的优先级函数,然后根据实际的姿态控制系统,设计了遗传算法的性能指标函数和具体的优化策略,最后给出了模糊PID控制器的设计思路。仿真结果说明了该方法的有效性。