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791.
干扰对组网雷达目标跟踪系统模型的影响,决定了系统需要用非线性滤波技术进行纯方位跟踪.粒子滤波避免了传统非线性滤波方法的缺陷,但是存在粒子退化,于是用EKF和UKF在每一时刻更新粒子,用更新的粒子及其协方差构造重要性函数,然后重采样.仿真实验表明了这两种改进粒子滤波方法的有效性.  相似文献   
792.
以双基地雷达"四抗"能力分析为基础,提出了双/多基地雷达布站优化的原则并对这些原则进行了量化,建立了双/多基地雷达布站优化的数学模型.随后,对量子粒子群算法进行了改进,提出了自适应量子粒子群算法,并将其用于双/多基地雷达布站优化数学模型的求解,解决了双/多基地雷达雷达站的部署问题.最后,通过MATLAB对优化后的雷达站...  相似文献   
793.
794.
压气机轮盘低循环疲劳寿命受很多随机参数的影响,具有很大的分散性,因此,对压气机盘低循环疲劳寿命进行稳健性设计具有重要的意义.在对疲劳寿命概率分析的基础上,结合RBF神经网络与混沌粒子群优化算法,利用混沌粒子群优化的动态收缩搜索区域的搜索特性,通过对随机参数进行优化进行压气机轮盘低循环疲劳寿命稳健性优化设计,使得疲劳寿命对参数的敏感度降低,概率区间减小,计算结果验证了该方法在工程应用中的可行性.  相似文献   
795.
多因素耦合复杂飞行情形风险定量评估方法   总被引:2,自引:1,他引:1  
多不利因素耦合诱发飞行事故具有隐蔽性强、因素关联复杂及状态"不可逆"性等特点,对其进行定量建模及风险评估研究难度较大。为此建立了典型装备故障和恶劣环境两类不利因素的定量数学模型。基于飞机六自由度全量运动方程、不利因素数学模型和人在环的操纵方式,应用MATLAB/Simulink、C语言和Flightgear软件开发了用于多因素耦合飞行情形研究的虚拟试飞安全性分析系统。建立了基于改进粒子群算法的极值分布风险评估模型,通过广义极值分布参数优化自动找到最为符合的极值分布模型。提出了随机自适应进化粒子群优化算法(RAE-PSO)对拟合过程进行优化,提高了评估精度和收敛速度。建立了多因素耦合复杂飞行情形的综合评估模型,以GJB 626A-2006中的试飞风险科目为例进行风险评估与结果分析,验证了方法的可行性和有效性。  相似文献   
796.
A novel target detection approach based on adaptive radar waveform design   总被引:2,自引:2,他引:0  
To resolve problems of complicated clutter, fast-varying scenes, and low signal-clutterratio (SCR) in application of target detection on sea for space-based radar (SBR), a target detection approach based on adaptive waveform design is proposed in this paper. Firstly, complicated sea clutter is modeled as compound Gaussian process, and a target is modeled as some scatterers with Gaussian reflectivity. Secondly, every dwell duration of radar is divided into several sub-dwells. Regular linear frequency modulated pulses are transmitted at Sub-dwell 1, and the received signal at this sub-dwell is used to estimate clutter covariance matrices and pre-detection. Estimated matrices are updated at every following sub-dwell by multiple particle filtering to cope with fast-varying clutter scenes of SBR. Furthermore, waveform of every following sub-dwell is designed adaptively according to mean square optimization technique. Finally, principal component analysis and generalized likelihood ratio test is used for mitigation of colored interference and property of constant false alarm rate, respectively. Simulation results show that, considering configuration of SBR and condition of complicated clutter, 9 dB is reduced for SCR which reliable detection requires by this target detection approach. Therefore, the work in this paper can markedly improve radar detection performance for weak targets.  相似文献   
797.
Our current understanding of the acceleration of solar-energetic particles is reviewed. The emphasis in this paper is on analytic theory and numerical modeling of the physics of diffusive shock acceleration. This mechanism naturally produces an energy spectrum that is a power law over a given energy interval that is below a characteristic energy where the spectrum has a break, or a rollover. This power law is a common feature in the observations of all types of solar-energetic particles, and not necessarily just those associated with shock waves (e.g. events associated with impulsive solar flares which are often described in terms of resonant stochastic acceleration). Moreover, the spectral index is observed to have remarkably little variability from one event to the next (about 50%). Any successful acceleration mechanism must be able to produce this feature naturally and have a resulting power-law index that does not depend on physical parameters that are expected to vary considerably. Currently, only diffusive shock acceleration does this.  相似文献   
798.
应用激光相位-多普勒系统测量雾化液滴颗粒和流动特性   总被引:1,自引:0,他引:1  
在几何光学近似理论的基础上分析了相位多普勒方法的理论模型和相位 粒径特性关系 ,分析了实验应用的光纤型激光相位多普勒系统的原理和组成 ,并应用此系统对雾化喷嘴的流动和颗粒特性进行了测量 ,得到了液滴的二维速度与粒径的相关和统计特性。  相似文献   
799.
One of the major topics of space weather research is to understand auroral structure and the processes that guide, accelerate, and otherwise control particle precipitation and during substorms. The problem is that it is not clear the structure of the magnetic field-aligned electric fields and how they are supported in the magnetospheric plasma. The objective of this research is to study the physical mechanisms of these phenomena in a laboratory experiment. It should be achieved by simulating the charged particle acceleration due to field-aligned electrical field generation in all totality of the interconnected events: generation of a plasma flow, its evolution in the magnetic field, polarization of plasma, generation of the field-aligned currents, development of instabilities in the plasma and current layers, double layers or anomalous resistance regions appearance, electron acceleration. Parameters of the laboratory simulation and preliminary results of the experiment are discussed.  相似文献   
800.
When the impact risk from meteoroids and orbital debris is assessed the main concern is usually structural damage. With their high impact velocities of typically 10–20 km/s millimeter or centimeter sized objects can puncture pressure vessels and other walls or lead to destruction of complete subsystems or even whole spacecraft. Fortunately chances of collisions with such larger objects are small (at least at present). However, particles in the size range 1–100 μm are far more abundant than larger objects and every orbiting spacecraft will encounter them with certainty. Every solar cell (8 cm2 area) of the Hubble Space Telescope encountered on average 12 impacts during its 8.25 years of space exposure. Most were from micron sized particles.  相似文献   
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