无线编码解码控制系统的设计与实践

通过无线电信道传输编码信号，以异频双工的方式实现无线电遥控与检测。主机向分机传送编码控制信号，分机从接收信号中解调出控制指令用以控制继电器工作，并同时把继电器所控制的用电器工作状态，通过监控信道传回主机实现检测。该系统还可实现双向同时遥控。     

应答式无线报警系统

应答式无线报警系统是一套规范化无线报警设备,它采用了MCS—51单片微机作为控制,从而使系统具有电路简单、性能可靠、控制灵活、成本低廉、操作简单、信息指示直观明了等特点,具有较强的科学性和先进性。     

近地告警系统报警阈值算法研究

近地告警系统的报警阈值的设定是研究告警系统技术过程中的一个重要问题。本文给出一种状态空间下的基于报警系统复杂性能指标的报警阈值的设计方法,该方法利用预先定义的包含不确定因素的轨迹模型,权衡报警和无报警之间的关系,以此来设定合适的报警阈值;最后,以近地告警系统模式1的阈值设置为例,在MATLAB环境中用Monte Carlo方法进行计算机仿真,验证了该报警系统阈值的设计方法。     

周界报警系统在民航机场中的应用

一、概述周界报警系统是飞行区安全防范的第一道屏障,是通过设置在物理围界上的报警传感器收集报警信息,通过联动广播系统、监控系统、灯光系统实施分区自动广播、报警现场录像、启动灯光等动作的一套飞行区安全防范系统。     

居住建筑燃气报警系统的设计应用

针对民用住宅楼中如何安全使用燃气、保障人民生命财产的问题,提出配备一套燃气报警系统．燃气浓度一旦达到设定报警值,系统就发出警报并自动切断气源,启动通风设备及燃气报警系统的保障安全措施。     

民航气象信息网监控系统

随着气象中心业务的发展及计算机和计算机网络的广泛应用,民航北京气象中心计算机室逐步担负起越来越重的业务工作。传统上一个对业务熟练的计算机工作人员完成一次日常对整个业务系统的检查,其过程复杂,时间较长,实时性不好,偶尔在操作中会遗漏对某项指标的检查。所以,为了更有效地管理整个业务网络运行系统,减少入力,促进民航气象应用自动化程度,及时了解在网各气象系统的主要信息,科学化管理业务系统的运行,特设计了本监控系统。     

消防自动报警系统的前期管理

本文介绍了楼宇建设过程中，针对消防自动报警系统的一些管理措施，目的是为了提高消防安装工程质量，确保消防系统在楼宇建成后能正常运转，使消防自动报警系统真正成为大楼安全的保护神。     

机载环境报警系统及其发展

近地警告系统（GPWS）、交通警戒与防撞系统（TCA）和风切变探测系统均为机载环境报警系统,它们是防止飞机撞地事故、避免和防止空中飞机相撞事故和避免风切变引起的事故的有效设备,对保障飞行安全,作出了重大贡献。这三种机载环境报警系统的报警优先顺序为：第一风切变;第二GPWS;第三TCAS。一、交通警戒的防撞系统（TCAS）1996年,墨西哥航空公司的一架客机在塞里托斯上空与一架小型飞机相撞后,有82人丧生,因而美国国会下令美国所有3O座以上的客机都要安装TCASZ设备。美国联邦航空局（FAA）也要求10－3O座的客机在1995…     

多载波调制结合Turbo编码技术的性能分析

多载波调制是一种有效克服衰落信道频率选择性的技术,从而显著减少码间干扰(ISI)。Turbo码以其接近香农极限的工作性能受到人们的注目,它能在极低信噪比条件下提供可靠通信。把多载波调制与Turbo 编码结合起来能够对整个系统提供显著的性能增益。本文试图对采用这两种技术的通信系统给出性能上的评估。     

一种实用的Turbo码编译码设计

Turbo码对解决远距离微弱信号处理问题提供了良好的途径,然而其交织器对存储的要求和译码算法的复杂性,提高了其工程实现的难度。本文提出一种实用的方案,采用二次置换多项式（QPP）交织器和线性拟合Log—Map译码算法,减少了计算量,节省了存储空间。同时,通过参量优化设计,提高了纠错性能。仿真实验结果表明,该方案能够满足低信噪比条件下的误码率要求,易于工程实现。     

一种针对高光谱图象识别与分类的二进编码方法

针对高光谱遥感图像中地物识别与分类问题,在对传统二进编码方法的优缺点进行分析的基础上,给出了一种新的二进编码策略,并给出了相应的快速匹配算法。该算法原理简单,易于实现,能够提高不同地物的可分性,试验结果表明,算法可以得到较好的分类效果。     

多分辨率分析及其在图像分解和编码中的应用

多分辨率分析是信号处理特别是图像处理的一种新的有效方法,可以在不同尺度上给出信号的信息。在分析其理论的基础上,将其应用在图像的分析的编码中,最后给出了处理结果。     

一种低噪声和高精度的频率合成技术

介绍了锁相环(PLL)技术和直接数字式频率合成(DDS)技术的基本工作原理,给出了一种提高DDS输出频率精度及减小其相位截断误差的方法。     

Conceptual design and analysis of legged landers with orientation capability

The lander with orientation capability is of fundamental importance for the “Returning” mission because its body can be the base with a suitable launching angle for the ascender lifting off. This paper proposes the conceptual design and verification of Landers with Orientation Capability (LOCs). Firstly, the topological composition of the lander is analyzed and expressed in the form of Lie group, which provides the fundamental principle for the type synthesis of LOCs. Then, the type synthesis approach for designing LOCs is proposed, which includes designing the Equivalent Parallel Mechanism (EPM) and the auxiliary limbs. Numerous mechanisms of LOCs with two-dimensional rotational motions are obtained based on the type synthesis approach by developing and combining the EPMs and auxiliary limbs. Afterward, kinematics and Jacobian matrix of a typical legged lander are developed, the workspace is analyzed, singularity configurations are analyzed based on the wrench graph method, and finally, the orientation capability is analyzed. The pitch and yaw angle reach 17.5°, considering the permissible range of joints. The proposed types of LOCs offer potential candidate for the “Returning” mission of the exploration mission.     

弹性地基两端铰支输流管的模态和固有频率

根据对单元体受力分析推导出了弹性地基输流管道的振动微分方程,应用分离变量法和数值方法计算了弹性地基输流管道在两端铰支情况下的模态和固有频率。研究了固有频率与管道内输送流体流速之间的关系;重点讨论了弹性地基、质量比、轴向力对固有频率与流速之间关系的影响,结果表明这些系数对于输流管道的振动特性有显著的作用。     

Design and Simulation of Electro-hydrostatic Actuator with a Built-in Power Regulator

The electro-hydrostatic actuator (EHA) is a kind of power-by-wire (PBW) actuator that converts the electrical power into localized hydraulic power for flight control. By removing the central hydraulic power supply together with hydraulic pipes, an EHA's reliability and efficiency are greatly improved but its frequency width and stiffness decreased. To overcome the drawback, this article proposes a novel structure of EHA associated with a power regulator. Composed of a high-pressure accumulator and a proportional valve, it can store and harness the hydraulic power flexibly according to the changing control requirements. The concept of transferred volume is put forward to estimate the capability of the power regulator. The actuator output position can be kept fixed with a hydraulic lock. The compounded control is specially developed to ensure the actuator system to operate in a correct manner. The simulation results indicate that the new-brand actuator results in efficient expanding of the system frequency width with an optimal power supply.     

Nonlinear flutter wind tunnel test and numerical analysis of folding fins with freeplay nonlinearities

The flutter characteristics of folding control fins with freeplay are investigated by numerical simulation and flutter wind tunnel tests. Based on the characteristics of the structures, fins with different freeplay angles are designed. For a 0° angle of attack, wind tunnel tests of these fins are conducted, and vibration is observed by accelerometers and a high-speed camera. By the expansion of the connected relationships, the governing equations of fit for the nonlinear aeroelastic analysis are established by the free-interface component mode synthesis method. Based on the results of the wind tunnel tests, the flutter characteristics of fins with different freeplay angles are analyzed. The results show that the vibration divergent speed is increased, and the divergent speed is higher than the flutter speed of the nominal linear system. The vibration divergent speed is increased along with an increase in the freeplay angle. The developed free-interface component mode synthesis method could be used to establish governing equations and to analyze the characteristics of nonlinear aeroelastic systems. The results of the numerical simulations and the wind tunnel tests indicate the same trends and critical velocities.     

Multi-objective optimization of frequency and damping of vertical stabilizer skin structure placed with variable-angle tows

The vibration characteristics of composite vertical stabilizer skin structures play a critical role in damping effects designed for overcoming the air disturbances experienced by aircraft structural components during flight. The first-order fundamental frequencies and their corresponding damping characteristics of the vertical stabilizer skin structure tow-steered by automatic fiber placement technique were optimized with the parameterized trajectories and plies as design variables. Firstly, the vibration and damping numerical models were derived based on Kirchhoff laminate theory, the Rayleigh-Ritz method, and the Strain Energy Method. Then the optimization model was developed by adopting the self-adaptive Differential Evolution Multi-objective optimization algorithm and incorporating the solution method of Pareto Front. The constraints of this optimization model considered the experimentally obtained minimum turning radius of prepregs tow-steered in automatic fiber placement process obtained from experimental tests. Finally, the comparison of numerical simulation results was conducted for the optimized trajectories and the conventional straight trajectories under various boundary conditions, and the numerical results were partially validated through damping and frequency tests. The results indicate the vibration characteristics of the composite vertical stabilizer skin structure can be enhanced to a large extent by optimizing fiber trajectories, and the enhancement percentage is affected by the boundary conditions of the actual structure.