遗传神经网络PID控制技术研究与应用

针对空调控制系统非线性、大滞后、时变性等特点,通过对中央空调总风量控制法的研究,提出了采用遗传算法神经网络PID控制方法,使空调控制系统具有较高的控制精度和良好的动态特性。仿真及实验结果表明该方法有效可行。     

The essential role of human spaceflight

The question is: should the United States and nations at large pursue a human spaceflight program (and if so, why)? I offer an unwavering positive answer to this question, and state the reasons for it while considering the broad challenges and benefits of (human) spaceflight. Space exploration is a human activity that is intrinsically forward-looking, and as such, has positive potential. Both national and international space programs can galvanize the population, inspire the youth, foster job-creation, and motivate the existing workforce. The nature of the enterprises involved—their scale, novelty, and complexity—requires a steady and continuous upward progression toward greater societal, scientific and technological development. That is, in order to overcome the challenges of human spaceflight, progress is required. More to the point, the survival of humanity depends on expanding beyond the confines of our planet. Human spaceflight, in short, presents us with an opportunity to significantly advance the nation and the global community.     

基于VHDL的I^2C总线IP核的设计

简述了I~2C总线的特点；并详细描述了一种在FPGA中实现I~2C总线IP核的设计方法；最后给出I~2C总线IP核在主模式下的收发数据仿真时序图以及实现结果。     

Study on Simulated Human Load in Unmanned Spaceship

This article introduces the methods for testing and verifying the performance of a new type of oxygen supply apparatus as well as the performance of the Environment Control and Life Support System(ECLSS)in the airtight unmanned space capsule,with a simulated human load instead of animals or human in China's Manned Space Program.The simulated human load also supplies a dummy for the spaceship to instal the envirmental testing equipment,to wear spacesuit,and to match the weight in spaceship.     

一种卫星数传分系统链路数据异常分析

某卫星数传分系统在轨测试初期,发现数传分系统的延时云图发射机(DPT)数传链路偶尔会有个别轨道接收数据异常.通过仔细观察发生问题时的各种现象,进行了产品地面试验的模拟和对数据的分析研究,找出了发生问题的原因.针对问题,对固态存储器内部时钟晶振加强了环境试验考核,对DPT时钟锁相环晶振电路加以改进完善,提高了电路的稳定性...     

基于复合优化的航空发动机模型参数估计

本文提出了一种复合优化方法,用于发动机多变量,状态空间模型的时域辨识。优化中粒子群优化算法和最小二乘优化算法按照“串联”方式运行。粒子群优化从一个初始种群出发,通过进化来搜索最优解。然而有些时候,粒子群算法会陷入次优解。那么最小二乘优化算法就可以从粒子群的次优解出发,通过共轭梯度法获得问题的最优解。本方法适用于待估计参数较多,且参数变化范围大的高阶多变量系统。本文将复合优化算法用于4输入4输出状态变量模型参数的估计。仿真结果表明了所提出方法的有效性。     

复合材料结构健康监测技术在飞机中的应用

结构健康监测(SHM)实现了工程结构设计与使用上的技术性跨越.将SHM应用于复合材料中,使得智能结构的设计与制造成为了现实.文章重点阐述了飞机复合材料结构SHM技术所面临的技术问题.SHM使飞机复合材料结构得视情维修以及降低其使用周期内成本成为可能,可以促使复合材料结构设计与制造的优化,最后指出了为实现复合材料SHMS所需要重点研究的理论与技术.     

民用飞机健康管理概念与系统研究

描述了飞机的健康状态,对民用飞机健康管理给出了明确的定义,概述了民用飞机的健康管理实施方案,介绍了民用飞机健康管理系统功能和信息分层.     

复杂系统体系结构设计方法研究

体系结构研究是认识复杂系统、控制系统复杂度的首要问题。复杂系统通常由多个具有交联关系的功能模块组成,各个模块之间通过相互作用组织起来,使系统具备特定的整体属性。随着系统复杂程度的增加,整个系统的组成结构、联结关系以及各个组成部分的规格说明显得越来越重要。与具体部件功能的实现技术相比,系统总体结构设计和组件规格描述相对重...     

A methodology to support strategic decisions in future human space exploration: From scenario definition to building blocks assessment

The human exploration of multiple deep space destinations (e.g. Cis-Lunar, NEAs), in view of the final challenge of sending astronauts to Mars, represents a current and consistent study domain especially in terms of its possible scenarios and mission architectures assessments, as proved by the numerous on-going activities about this topic and moreover by the global exploration roadmap. After exploring and analysing different possible solutions to identify the most flexible path, a detailed characterisation of several Design Reference Missions (DRMs) represents a necessity in order to evaluate the feasibility and affordability of deep space exploration missions, specifically in terms of enabling technological capabilities.The study presented in this paper was aimed at defining an evolutionary scenario for deep space exploration in the next 30 years with the final goal of sending astronauts on the surface of Mars by the end of 2030 decade. Different destinations were considered as targets to build the human exploration scenario, with particular attention to Earth–Moon Lagrangian points, NEA and Moon. For all the destinations selected as part of the exploration scenario, the assessment and characterisation of the relative Design Reference Missions were performed. Specifically they were defined in terms of strategies, architectures and mission elements. All the analyses were based on a pure technical approach with the objective of evaluating the feasibility of a long term strategy for capabilities achievement and technological development to enable future space exploration.This paper describes the process that was followed within the study, focusing on the adopted methodology, and reports the major obtained results, in terms of scenario and mission analysis.