Total information processor for 121.5/243 MHz SARSAT signals

Search and rescue satellite-aided tracking (SARSAT) has certain shortcomings which could possibly be ameliorated by employing a more extensive signal processing strategy. The approach proposed is based on partially compensating for the Doppler shift, which then permits the data processing windows to be increased significantly. Incorporating a ranking technique with the conventional fast Fourier transform (FFT) processor and implementing an autoregressive moving-average estimator provides an optimal strategy that maximizes the probability of detecting the emergency signals     

Interference in the 121.5/243 MHz SARSAT Frequency Bands

In the SARSAT signal environment it is possible to receive many(5 to 20) simultaneous emergency beacon signals combined with voice and interference of various types, all simultaneously occupying essentially the same frequency-time space. The paper first provides a survey of the different sources of interference which occur in the 100 to 500 MHz frequency band. Then the paper examines those sources of interference which enter the 121.5/243 MHz frequency bands of the SARSAT system.     

A new system identification technique for harmonic decomposition

An extended and unifying system identification technique is presented for a class of systems that include all main signal models that arise in the harmonic decomposition problem. This technique unifies and extends the previously developed system identification techniques which are improvements on the Pisarenko harmonic decomposition (or, its spatial dual, MUSIC) as they arise in arrays of sensors. The advantages of the technique and some of its specializations include having no assumptions of stationarity on the stochastic processes involved. Another contribution of this technique is that it can also be used without any resort to probability theoretic concepts, thus bypassing the approximation of autocorrelations via time averages, yielding the system parameters exactly. This technique can be utilized to determine the dominant modes of vibrations of flexible structures as well. An analogy is established between arrays of sensors for target signal returns and those that can be used for vibrations in flexible structures. This enables the results developed for each one of these problems to be applied to the other     

提取流管实验装置中声衬声阻抗的模态方法

发展了一种模态匹配方法进行有均匀流条件下敷设声衬的二维矩形流管中声传播的计算, 计算结果与NASA流管实验结果和CAA计算结果符合得很好.在此基础上, 着重介绍采用求极值的变尺度法优化目标函数和给定求解范围寻找目标函数最小值两种方法进行管内未知声阻抗的提取, 给出了算例验证, 并分析了随机误差和已知声压点数对计算结果的影响.      

A technique for selecting a rational variant of a multifunctional aircraft system

A technique for selecting a rational variant of a multifunctional aircraft system using the analytic hierarchy process is proposed and a solution of a practical problem is presented.     

A parametric synthesis technique for a stationary multichannel flow-type aerometric receiver in the helicopter air data system

The statement and a technique for solving a problem of parametric synthesis and rational choice of structural parameters for a stationary multichannel flow-type aerometric receiver using the results of the experiment being planned are clarified. The scheme of a design model and a receiver structure that provide an increase in noise immunity and extension of working velocities in the helicopter air data system are described.     

一种适用于FADEC系统的宽输入范围AC/DC变换器

针对航空发动机全权限数字电子控制(FADEC)系统专用发电机的输出特性,提出一种电流回馈型恒流变频AC/DC(交流/直流)变换技术,以适应专用发电机的宽输出范围,满足FADEC系统的供电需求.给出了该技术的控制策略、拓扑结构、工作原理、过压故障检测及保护设计方法.试验结果表明:该变换器工作稳定,在-55~125℃全温范围内,满足国家军用标准飞机供电特性(GJB181A)对电源的相关规定.研究成果已成功应用于某型航空发动机数字控制系统中,并通过了台架试车和飞行平台试验.      

带五分量抑制机构的高精度滚转力矩测量技术

滚转通道是飞行器控制的重要通道,且在试验中滚转单元受天平其它元干扰较大。为了准确测量滚转力矩,特别开发了带五分量抑制机构的高精度滚转测量技术。该技术设计原理是通过带机械深沟球轴承的抑制机构对除滚转力矩外的五个分量进行抑制。该技术一方面具有较高的滚转力矩测量灵敏度,另一方面能够有效抑制除滚转力矩外的其它五个分量,从而得到准确滚转力矩信号。     

发动机轴流压缩系统逐级模拟技术

基于轴流压气机逐级过失速特性,建立了一个能够显示压缩系统喘振和旋转失速等过失速行为的一维非定常逐级模拟技术,发展了分析轴流压缩系统过失速响应的动态滞后方法。并将该模型应用于国内某型号的高转速、双转子压缩系统的过失速行为的分析,讨论了时间滞止的常数、燃烧室对压缩系统失速行为的影响,得到了合理的定性结果。     

Ajax技术在Web开发中的应用

介绍了Ajax的原理和开发流程,给出了Ajax在Web开发过程中的一个应用实例。通过Ajax,可以使得客户端页面不需要被重新加载,用户不会感觉到有网页提交或刷新。在不刷新页面的情况下,页面仍然可以检索、查询并返回浏览者所输入的相关结果。     

A technique for formation of control and decision-making in the channels of the safety system of airborne ergatic complex operation

The mathematical statement and a technique for solving a problem on formation of control and decision-making in the off-normal situations with the use of informative functions of failure danger in the airborne ergatic complex elements are considered.     

A technique for calculating nonstationary processes in airbreathing pulse engines

A technique for calculating the performance of airbreathing pulse engines with the result accuracy about 20% has been developed. The results of comparison with other similar techniques are correlated with experimental data.     

A new technique for decoding Loran-C radionavigation signals

A new approach to the extraction of navigation information from Loran-C radionavigation signals is described. A reduced-rate time-reversed sequence is derived from the RF signal and processed by a finite-impulse response (FIR) filter. It is shown that proper design of the FIR filter and proper control of the sampling point guarantee the rejection of skywave contamination, and achieve excellent rejection of continuous-wave interference (CWI). The process is computationally efficient     

A technique for simulation of a fluid flow in branched channels

In this paper, a technique for simulation of the space-time flow parameters in branched channels under transient boundary conditions is presented. The technique is based on the solution of one-dimensional nonstationary equations of gas dynamics. We suggest the conditions of channel junction with regard for distinctive features of a fluid flow in the adjacent region and compare the data on the flow simulation in the channel with a lateral branch by using one-dimensional and three-dimensional models. Comparing the data obtained with the experimental results, we show that the technique being suggested adequately simulates the real processes in the branched channels.     

A 0535 + 26/HDE 245770: A typical X-ray/Be system

Among the X-ray/Be systems, A 0535 + 26/HDE 245770 has been noted, since its discovery, for its peculiar features in several respects, in a wide energy range. For this reason and for a series of concomitant favorable causes, this system has been one of the most studied among the massive X-ray binary systems. The most remarkable incident was that its optical identification with an early-type-emission-line star (O9.7IIIe) has led to a deep studies on Be stars and their interactions with neutron stars, which have allowed to discover, without unbiguity, the presence of optical indicators of consequent X-ray flares, as well as that Be stars in X-ray/Be systems behave just as normal Be stars. Overmore, thanks to the multifrequency coordinated observations of this system, the X-ray emissions from binary companion of the Be stars are best explained by assuming the presence of a thick equatorial disk with low expansion velocity and a thin polar region with high expansion velocity. This picture reconciled the strong discrepancy in mass loss rate evaluations coming from IR and from UV measurements, assuming that the observed regions are enterely distinct from each other, one being a high-density, low-velocity region, and the other being a low-density, very hot, rapidly-expanding disk-like zone.Since, this picture seems to be the best up-to-date frame to cuckold all the experimental panorama available on X-ray/Be systems, we would like to paint in this paper the multifrequency behaviour of A 0535 + 26/HDE 245770, which is the best studied among such systems, in order to stimulate future coordinated experimental-theoretical works on this very interesting class of objects.     

A fault-tolerant air data/inertial reference system

The air data inertial reference system (ADIRS) described consists of a fault-tolerant air data inertial reference unit, a secondary air data attitude reference unit, and six air data modules. The ADIRS replaces the conventional inertial reference and air data systems and uses ARINC 629 bi-directional serial digital data bus interfaces. The ADIRS is designed to be the inertial and air data reference for the ARINC 651 integrated modular avionics (IMA) distributed architecture and provides low life cycle cost and high availability through high reliability, simple high integrity monitoring and deferred maintenance     

A novel pulse TOA analysis technique for radar identification

A new processing technique is presented for identifying individual pulse trains in a buffer load of pulse time-of-arrival (TOA) data from radar warning receiver sets currently in use for electronic warfare (EW). The method is based on the numerical characteristics of the matrix of the differences of the TOA data points. In particular, for a uniform pulse repetition interval (PRI) emitter, this matrix is a symmetrical harmonic Toeplitz matrix the inverse of which has banded tridiagonal form. This form leads to an estimator for the PRI in terms of the trace of the inverted matrix     

激波/湍流边界层干扰的流动控制技术

激波/湍流边界层干扰(STBLI)是航空航天领域中广泛存在的一种复杂流动现象,形成条件涵盖跨声速到高超声速,形成环境复杂多样,给飞行器的气动性能和结构安全性带来重大的影响。结合STBLI的典型流动图像介绍了干扰区的重要物理特征;总结了一些有代表性的STBLI流动控制技术的现状,分析了包括涡流发生器、电磁激励等控制技术的原理、效果及不足;探讨了STBLI流动控制研究中有待于进一步深入研究的问题和方向,为发展实用、高效、针对高超声速条件下的STBLI流动控制技术提供了理论支撑和技术储备。     

高超声速风洞多体干扰与分离试验技术

在FL-31风洞中进行了某高超声速飞行器的多体干扰与分离试验技术研究,成功建立了多体干扰与分离试验技术。试验模型是某典型构型的可重复使用航天飞行器,由助推器以及再入体两部分组成。利用风洞上下投放机构实现两模型间的相对运动,采用两台天平对模型的气动力进行测量,同时利用纹影仪记录模型分离过程中的激波干扰情况。结果表明：试验系统设计合理,能准确模拟物体间分离过程,并能精确测量多体干扰的气动力特性,激波干扰清晰可见。     

A technique for selecting optimal engineering decisions in gas turbine plant design

A technique for evaluating the preferential usage of one or the other engineering decision is presented; for this, the objective function that represents the comparative profit of future GTP owners from realization of alternative power plant variants is used. The efficiency of the approach being proposed is shown by analyzing the possible modifications of the Siemens GT10C and GTX100 gas turbine plants operating in the Russian Federation.