导弹武器系统项目前评价体系研究

阐述了对导弹武器系统项目中诸如风险、费用、可靠性、维修性及效能等方面进行评价的重要性,根据指标选取的原则,建立了评价指标体系的框架。在此基础上进一步说明了框架中的各项指标,并细化了各分项指标,形成了一个完整的评价指标体系。最后,对评价中可能用的方法及模型的建立思路给出了初步构想。     

民机驾驶舱触控显示系统人机工效评估指标体系搭建研究

从人机工效基本原理出发,在对国内外适航规章和行业标准解读的基础上,结合触控技术自身特征,对触控显示系统人机工效设计的影响因素进行分析,并综合运用了改进德尔菲法和改进层次法,初步构建了民机触控显示系统人机工效评估指标体系,可为系统的设计与评估提供借鉴.     

舰载直升机系统安全评价指标体系

为了准确地对舰载机系统进行安全分析，确定客观的安全评价指标，文章选择“人、机、环境、管理”4个方面共29个评价指标，这些指标基本涵盖了舰载机系统的安全评价所包含的有效信息。利用模糊聚类的方法再对该指标体系进行筛选，最终确定了精简且具有科学性的指标体系。     

Ionospheric climate index as a driving parameter for the NeQuick model

Ionospheric delay is one of the significant error sources for global navigation satellite system (GNSS) positioning. GNSSs broadcast the coefficients of the ionospheric model to correct ionospheric delay for single-frequency users. A modified three-dimensional model (NeQuick G) based on the NeQuick climatological model is adopted for Galileo users. The NeQuick G model uses the effective ionization level (Az) instead of the sunspot number as the driving parameter. In this study, we introduce the ionospheric climate index (ICI) as a new driving parameter for the NeQuick model. In comparison, the ICI-driven NeQuick model has a better performance than the Az-driven NeQuick G model at both low and high latitudes. In addition, only one GNSS station at low latitudes is required to calculate the ICI, which would save maintenance costs and improve the efficiency of updating the broadcast coefficients. This model has potential application value for future upgrades of Galileo’s ionospheric broadcast model.     

Decline of geomagnetic and ionospheric activity at earthquake during spotless Sun

We investigate the geomagnetic and ionospheric effects of seismic activity during 1954 Sun spotless days (SSL) from 1995 to 2020. Two subsets of earthquakes (EQ) are evaluated for 676 events observed with the depth D1 ≤ 30 km and 1278 events with D2 > 30 km and the total set SSL. Newly developed 1 h geomagnetic index Hpo and the ionospheric W_EQ index are used for the comparisons with the daily peak earthquake. The ionosphere W_EQ index is derived at the EQ epicenter from JPL GIM-TEC map within the cell of 2.5°×5°, in latitude φ and longitude λ surrounding the epicenter at radius of about 200 km. We use the method of superposed epoch with the zero epoch time t₀ taken at EQ to extract peak values of Hpo and W_EQ during t₀-24 h ≤ t < t₀ (preEQ) and t₀ < t ≤ t₀ + 24 h (postEQ). It is found that the magnitude of Hpo(t₀) is less that the both peaks of Hpo(preEQ) and Hpo(postEQ) in 91 % of events independent of EQ’s depth. Similar effect is observed with the peak of the positive/negative ionosphere indices and the absolute values of |W(preEQ)| and |W(postEQ)| the both exceeding |W_EQ| in 77 % of events. The seismic activity tends to increase towards the solar minimum when SSLs occur. Our results provide evidence that EQ-related geomagnetic and ionospheric activities experience decline of intensity at the time of EQ under SSL.     

反舰导弹项目评价系统设计

在对反舰导弹项目所涉及的各方面进行充分分析的基础上,建立了包括必要性、可行性、经济性、实用性、先进性和保障性方面的指标体系,并据此建立了反舰导弹项目评价的指标体系.根据评价方法选取原则,针对建立的评价指标体系选取了8种方法,在编程实现过程中,采用了改进的专家评分法、模糊方法和数据处理方法等,增加了对数据的利用率,在一定...     

指数法在反舰导弹武器作战能力评估中的应用

指数法是一种定量评价事物属性的方法，文中分析了影响反舰导弹武器系统的能力层次结构，并在此基础上介绍了运用指数法评估反舰导弹武器作战能力的方法。     

增强神经网络辨识模型泛化能力的研究

神经网络(Artificial Neural Network,ANN)辨识模型的泛化能力是其最主要的性能之一,增强ANN模型的泛化能力也是近年来国内外有关专家学者研究的重点问题。大量研究表明,ANN模型泛化能力的改善与很多因素相关联,其中恰当的性能指标函数设计是一个重要影响因素。文中在分析常见的基于均方误差最小原则的性能指标函数基础上,通过加入ANN辨识模型权值间的延迟信息,进而获得一种改进型性能指标函数。通过仿真,验证了所设计的改进型性能指标函数对增强ANN辨识模型的泛化能力是有效的。     

Parameter optimization for torsion spring of deployable solar array system with multiple clearance joints considering rigid–flexible coupling dynamics

In this paper, four novel evaluation indices and corresponding hierarchical optimization strategies are proposed for a deployable solar array system considering panel flexibility and joint clearance. The deployable solar array model consists of a rigid main-body, two panels and four key mechanisms, containing torsion spring mechanism, closed cable loop mechanism, latch mechanism and attitude adjustment mechanism. Rigid and flexible components are established by Nodal Coordinate Formulation and A...     

Optimum alternate material selection methodology for an aircraft skin

Weight penalty has been a challenge for design engineers of aerospace vehicles. Today’s high-efficiency combat aircraft undergoes intense stress and strain during flying missions, which require stronger and stiffer materials to retain structural integrity. Though metallic materials have been successfully used for the construction of aircraft structures and components, metals still have a low strength-to-weight ratio. This paper aims to develop an alternate optimised material selection methodolog...