Validation of B2bot in the NeQuick model during high solar activity at Hainan station

NeQuick ionospheric electron density model, which has been developed to version 2, produces the full electron density profile in the ionosphere. Each part of the profile is modeled using Epstein layer formalism. Simple empirical relations are used to compute the thicknesses of each layer. In order to validate the B2_bot parameter in the NeQuick model during high solar activity, we use the data at Hainan, China (109.1°E, 19.5°N; Geomagnetic coordinates: 178.95°E, 8.1°N), measured with DPS-4, and study the diurnal and seasonal variations of B2_bot, ΔB2 (B2_best − B2_NeQuick 2) and the seasonal median values of B2_best/B2_NeQuick 2 at that region. The results show that, (1) The differences between B2_best and B2_NeQuick 2 have diurnal and seasonal variations. (2) The diurnal variations of B2_NeQuick 2 are smaller than those of B2_best. (3) Generally, except for early morning the experimental values are properly reproduced. (4) Generally, during morning the NeQuick model has an underestimation. The magnitude of underestimation varies with LT and season.     

An update global model of hmF2 from values estimated from ionosonde and COSMIC/FORMOSAT-3 radio occultation

In this paper, we present our recent work on developing an updated global model of the ionospheric F2 peak height hmF2 parameter by combining data from the Constellation Observing System for Meteorology, Ionosphere and Climate (COSMIC/FORMOSAT-3) radio occultation (RO) measurements and from the extended global ionosonde stations. In particular, 10 Chinese ionosonde stations’ data are newly introduced into this study. The modeling technique used is based on a two-layer empirical orthogonal function (EOF) expansion. Global distributions of hmF2 maps calculated using the newly constructed global model and the one provided by the International Reference Ionosphere model (IRI-ITU-R) are compared with the global distributions of hmF2 obtained by the COSMIC RO measurements and quantitative statistical analysis of the differences between the model results and those of the COSMIC RO measurements is made for the low (2008) and high (2012) solar activity years. The obtained average root-mean-square differences (RMSEs) for our model are 27.7 km (11.1%) and 31.0 km (9.8%), respectively for the years 2008 and 2012, whereas those for the IRI-ITU-R model are 39.9 km (16.9%) and 35.0 km (11.6%), respectively. Comparison of the results calculated both by our model and the IRI-ITU-R model with the digisonde observation is also made. The comparisons show that the newly constructed global hmF2 model can reproduce reasonably well the observations and perform better than IRI-ITU-R model.     

Evaluation of global modeling of M(3000)F2 and hmF2 based on alternative empirical orthogonal function expansions

Global modeling of M(3000)F2 and hmF2 based on three alternative EOF (empirical orthogonal function) expansion methods is described briefly. Data used for the model construction is the monthly median hourly values of M(3000)F2 from the ionosonde/digisonde stations distributed around the world for the period of 1975–1985 and the hmF2 data of the same period converted from the measured M(3000)F2 based on the strong anti-correlation existing between them. Independent data of a low (1965) and a high (1970) solar activity year are used to validate the three alternative models based on different EOF expansion methods. Comparisons between the modeled results and observed data for both the low (1965) and high (1970) solar activity years showed good agreement for both M(3000)F2 and hmF2 parameters. Statistical analysis on the differences between model values and observed data showed that all the three alternative models (Model A, B and C) based on the different EOF expansion methods have better agreement with the observed data than the models currently used in IRI. All three alternative EOF based models have almost the same accuracy. Discussion on the preference of the three alternative EOF based models is given.     

轻型直升机起落架的载荷分析与设计

轻型直升机的滑橇式起落架结构简单,有着广泛的实际应用。本文针对某项目直升机的设计需要,用机械能守恒定律和材料力学的方法对该型起落架的着陆载荷做出定量分析,并校核了起落架的垂直过载和强度。     

Global empirical models of the density peak height and of the equivalent scale height for quiet conditions

Monthly average electron density profiles have been calculated from hourly electron density N(h) recorded in 26 digisonde stations distributed worldwide encompassing the time interval 1998–2006. The ionospheric electron density peak height of the F2 region, hmF2, and the effective scale height at the hmF2, Hm, deduced from average profiles have been analyzed to obtain the quiet-time behavior and have been analytically modeled by the spherical harmonic analysis (SH) technique using the modip latitude as the coordinate of the reference system. The coefficients of the SH models of hmF2 and Hm are bounded to the solar activity, and the temporal and seasonal variations are considered by Fourier expansion of the coefficients. The SH models provide a tool to predict hmF2 and Hm located anywhere in the range of latitudes between of 70°N and 70°S and at any time. The SH analytical model for hmF2 improves the fit to the observations by 10% in average compared to the IRI prediction, and it might improve the IRI prediction of hmF2 by more than 30% at high and low latitudes. The analytical model for Hm predicts the quiet behavior of the effective scale height with accuracy better than 15% in average which enables to obtain a good estimation of vertical profiles. These results could be useful to estimate information for the topside profile formulation.     

高超声速滑翔飞行峰点高度确定方法

针对快速准确获取高超声速滑翔峰点高度的问题,提出了一种在给定初始速度大小的情况下峰点高度计算的迭代算法.考虑将动压和过载约束条件统一到热流率约束条件上,首先在常数速度条件下估算了峰点高度,然后依据峰点高度容许误差迭代计算了峰点高度的修正值,最后通过算例进行了验证.仿真结果表明,该算法计算速度快、精度高,具有同时处理三种约束条件的通用性.     

反舰导弹控制中的稳定性研究

应用零动态和精确线性化理论，对反舰导弹的几种控制方法进行了研究。研究表明，姿态控制系统和传统的加速度控制系统都是最小相位系统，但纯加速度控制系统却是一种非最小相位系统。最后，对过载控制系统也进行了稳定性研究，表明它是最小相位系统，从而解决了纯加速度控制的非最小相位问题。     

基于积分滑模的导弹过载控制稳定性研究

针对导弹过载控制系统,考虑了导弹舵机的一阶动态特性,引入一类积分型滑模面,设计变结构控制律,对导弹的过载和角加速度进行控制。然后构造Lyapunov函数证明其稳定性,仿真算例表明了该方法有较好的鲁棒性和快速性。在此基础上,考虑工程应用的需要,提出了一种形式简单的控制规律,减少了控制信号的计算量,仿真结果表明,该控制律具有优良的控制效果。     

卫星自主完好性相关峰监视

卫星自主完好性监测（SAIM）技术是地面完好性监测手段的重要技术补充,可以有效缩短告警时间,有助于从根本上提高完好性性能。从SAIM技术出发提出多通道相关峰监测算法,实现多点异步采样,恢复相关峰。通过MATLAB软件仿真验证算法并给出典型异常模型及监测结果,并用普通接收机验证工程可实现性。通过软件仿真和实测结果对比论证了方法的可行性,采用成熟的商业星载接收机进行软件修改有效地降低了卫星完好性接收装置的研发难度。     

脉冲激光热传导焊接技术在石英挠性加速度计 组件装配连接上的应用研究

在不改变激光重复频率、焊接速率、脉冲宽度、离焦量等参数的情况下,只改变峰值功率,采用Nd:YAG脉冲激光对石英加速度计表芯装配组件进行热传导焊接,通过X射线显微镜和超声波无损检测系统对焊接样件的焊缝形态与焊接质量进行检测分析,并对样件拉伸强度进行测试.结果表明:脉冲激光热传导焊接中的热输入量对焊缝形态和焊接质量有直接的影响,较低的热输入量可以实现边界轮廓整齐、表面光亮、热影响区较小、残余应力较低的焊缝形态,并且没有裂纹缺陷,同时焊接样件的拉伸强度是环氧胶粘接样件的3倍以上.因此,脉冲激光热传导焊接技术在组件装配连接上的应用具有潜在的优势.