基于C8051F020单片机的无人机加速度采集系统

为了满足无人机三轴加速度测量与控制的需要,设计了一种简易、方便的加速度采集系统.本系统采用高集成度单片机C8051F020进行多通道数据的采集和A/D 转换,在单片机内部完成数据存储、数据处理,再利用串行通信接口将数据传送至上位机,然后由无线发射模块发送至地面接收设备.在试验条件下,可以将采集到的数据传送至PC机进行分析或者由液晶显示仪显示.     

双曲梁传感器推力测量技术应用

为提高小推力发动机的测量精度,对原测量误差大、测量结果易受环境情况影响的应变梁推力测量装置进行了改进。改进后采用双曲梁推力测量系统。从安装、校准等方面介绍了系统的改进措施及实际应用情况。试验结果表明,双曲梁推力测量系统测量精度高,内阻输出低、抗电干扰性能好。     

噪声干扰Link-16数据链的干扰功率分配方法

在建立对Link-16数据链的干扰模型和接收机模型的基础上,分析了噪声干扰下接收机的误码性能,研究了干扰功率分配问题,并得到了对Link-16数据链的干扰功率分配方程,最后进行了仿真分析。     

基于平均相位增量法的多普勒中心估计方法研究

为了实现高分辨率成像,在保证系统实时性的同时还要保证中心频率估计的精度。研究了利用平均相位增量法精确估计多普勒中心的仿真实现过程,并利用这种方法对实测数据进行了中心估计和成像,取得了较好的效果。     

电磁脉冲作用下计算机死机故障研究

为研究核电磁脉冲对计算机系统的效应,利用核电磁脉冲源产生的模拟核电磁脉冲,对单片机系统进行了辐照效应实验。实验表明,单片机系统在核电磁脉冲作用下,可出现死机等多种故障现象。在实验的基础上,分析了死机产生的原因及加固方法,并通过实验验证了指令冗余、软件陷阱和看门狗等措施对防止单片机死机的有效性。     

航空发动机环形燃烧室噪声总声级的GMDH方法研究

采用数据处理的组合方法（GMDH）,研究航空发动机环形燃烧室测试数据。通过简单的二元二次回归原理来构造出下一代较为复杂的次级回归方程,并且利用＂优选原理＂淘汰掉次级回归方程中的那些不理想的项,得到燃烧室噪声总声级的高阶方程,获得较客观的描写复杂非线性系统的非线性模式。     

构建支撑行业发展的民航科学数据体系

民航科学数据作为民航科技、管理、生产活动产生的原始、基础和分析研究信息,具有巨大的价值。建立民航科学数据体系,实现民航科学数据共享,是民航科技创新体系建设的重要组成部分。本文在研究中国民航科学数据现状和需求基础上,提出了面向全民航的科学数据共享体系,并介绍了民航科学数据中心建设的进展状况。     

Pioneer 10 Doppler data analysis: Disentangling periodic and secular anomalies

This paper reports the results of an analysis of the Doppler tracking data of Pioneer probes which did show an anomalous behaviour. A software has been developed for the sake of performing a data analysis as independent as possible from that of Anderson et al. [Anderson, J., Laing, P.A., Lau, E.L., Liu, A.S., Nieto, M.M., Turyshev, S.G. Study of the anomalous acceleration of Pioneer 10 and 11. Phys. Rev. D 65, 082004, 2002], using the same data set. A first output of this new analysis is a confirmation of the existence of a secular anomaly with an amplitude about 0.8 nm s⁻² compatible with that reported by Anderson et al. A second output is the study of periodic variations of the anomaly, which we characterize as functions of the azimuthal angle φ$\phi$ defined by the directions Sun–Earth Antenna and Sun-Pioneer. An improved fit is obtained with periodic variations written as the sum of a secular acceleration and two sinusoids of the angles φ$\phi$ and 2φ$2\phi$. The tests which have been performed for assessing the robustness of these results are presented.     

Tomographic reconstruction of the ionospheric electron density as a function of space and time

Electron density distribution is the major determining parameter of the ionosphere. Computerized Ionospheric Tomography (CIT) is a method to reconstruct ionospheric electron density image by computing Total Electron Content (TEC) values from the recorded Global Positioning Satellite System (GPS) signals. Due to the multi-scale variability of the ionosphere and inherent biases and errors in the computation of TEC, CIT constitutes an underdetermined ill-posed inverse problem. In this study, a novel Singular Value Decomposition (SVD) based CIT reconstruction technique is proposed for the imaging of electron density in both space (latitude, longitude, altitude) and time. The underlying model is obtained from International Reference Ionosphere (IRI) and the necessary measurements are obtained from earth based and satellite based GPS recordings. Based on the IRI-2007 model, a basis is formed by SVD for the required location and the time of interest. Selecting the first few basis vectors corresponding to the most significant singular values, the 3-D CIT is formulated as a weighted least squares estimation problem of the basis coefficients. By providing significant regularization to the tomographic inversion problem with limited projections, the proposed technique provides robust and reliable 3-D reconstructions of ionospheric electron density.     

基于Flowmaster的运输机供氧系统仿真

研究运输机供氧系统,建立相应的系统仿真模型,对整个管网系统中氧气的流动及分配进行仿真分析.系统由高压氧源、机组供氧点和座舱乘员供氧点3部分组成,各部分分别建模,然后集成系统;为了方便设计者针对不同的管路布置进行系统仿真分析,利用Flowmaster的外部元件模块开发出了氧气系统特有的元件,包括氧气调节器、减压器和快戴式氧气面罩;在某任务航程下利用此仿真模型对氧气系统进行了仿真计算,得到各气瓶耗氧量和各供氧点氧气流量的变化情况,验证了系统是否满足设计需求.