做好信息化工程监理的体会

阐述信息化工程设计分为硬件、软件两部分;系统建设(集成)阶段质量的事前控制重点是实施方案审定和统一验收标准,事中和事后控制的重点和难点是系统测试;政府投资的信息化项目进度控制上的特点;信息化工程监理需要复合型人才。     

新氢脉泽频率标准的支持电子学系统

氢脉泽的支持电子学系统是氢脉泽频率标准中子学的一个重要组成部分，它包括脉泽的热控制、磁场控制、氢压以及调谐控制。本将介绍上海天台新近研制成功的新氢脉泽（H7）的支持电子学系统的各控制部分的设计思想及特点。     

混凝土试件质量监理控制要点

加强对混凝土试件的留置、养护、试验管理是工程质量控制的关键项目,也是监理工程师质量控制的重要内容。     

基于RTS2和EPICS的成像控制软件的设计

EPICS是一个用于开发分布式设备控制程序的软件开发框架,它主要用于控制大型物理实验设备及天文望远镜系统,而RTS2是Linux系统上的一个远程自主望远镜控制系统。实现了EPICS与RTS2的集成,用RTS2负责望远镜观测流程控制,EPICS用于成像设备控制,使用EPICS的成像控制软件Area Detector完成了Andor相机的控制,并完成了RTS2和EPICS融合的命令状态接口,从而让RTS2能够兼容EPICS组件。成功用RTS2和EPICS实现了Andor相机的控制,并很好地集成到RTS2的流程控制中。     

浅析公路工程监理中的费用控制

费用控制直接关系到业主和承包商的利益。影响费用控制的关键环节在于路基清表后横断面的测绘、计量红线的核定、土石分界的确定、工程变更处理、议价项目处理、索赔项目处理。     

拼接镜面主动控制系统的定标

对拼接主镜进行主动控制是拼接镜技术的难点之一,8 m环形拼接太阳望远镜主动光学的控制性能主要取决于倾斜探测的精度与控制模型建立的准确程度。在研制主动控制系统时,需要对倾斜探测精度定标以及建立较为准确的控制模型,即对主动控制系统定标。实验系统中搭建了用于实时探测拼接子镜倾斜的夏克-哈特曼波前传感器,并对其重复测量精度进行了定标,精度达到0.014 arcsec,接近8 m环形太阳望远镜面形控制的要求。然后利用边缘传感器和夏克-哈特曼波前传感器测量了两镜主动控制系统的控制矩阵,建立较为准确的控制模型。     

分布式望远镜控制系统的构想和实践

介绍了一种基于分布式控制思想的望远镜系统控制方案。使用这种控制方式可以大大简化望远镜电控系统的维护和改造工作，且扩展性强。我们通过在兴隆基地几台望远镜上的前期试验，在本中提出一个基于无线串口通讯的具体实施方案。     

40m天线预测控制算法的研究

将预测控制的思想用于大口径天线跟踪系统的控制,提出了位置控制器的一种设计方案。并对天线的直流驱动系统进行建模和仿真实验。     

一种低频时码接收机数字式自动增益控制的设计

为扩大低频时码接收机的输入动态范围,进行了数字式自动增益控制(AGC)的设计。详细介绍了低频时码接收机数字式自动增益控制的设计方法和实现原理,并进行了计算机仿真。仿真结果表明,该数字式自动增益控制是可行的,相对于没有实行自动增益控制的情况而言,大大增加了接收机的动态范围。     

一种用于天文望远镜支撑机构的并联机器人控制方案

针对一种用于天文望远镜支撑机构的6自由度的并联机器人,提出了基于预测机制的控制方案,描述了该机器人的结构和运动学,设计并实现了控制方案的具体功能,对控制过程的仿真结果进行分析,验证了控制方案的有效性.     

Study of central control system for FAST

FAST(The Five-Hundred-Meter Aperture Spherical Radio Telescope) is an under-building radio telescope which will be the largest single dish in the world. Through the study of the central control system, in accordance with the actual operation of the telescope and observation process, this article introduces the physical models for engineers and observers, the central control system architecture design, basic support modules and the necessary interfaces. We simulated observation control process and telescopes monitoring and control process, and took Active Reflector System as a subsystem example to complete the control system design and implementation using EPICS (Experimental Physics and Industrial Control System). The Central control system, with active reflector systems, feed supporting system has been taken to an integration test at Miyun model. In the case of the normal operation of the various sub-systems of the Miyun model by the central control system, a coordinated control is achieved.     

10m口径射电望远镜天线计算机远程控制系统

本文从当前天文观测所受自然环境的影响入手 ,提出远程控制观测是解决目前观测所遇到的困扰的好方法 ,并介绍了中科院云南天文台太阳射电组的 1 0m口径抛物面天线的计算机远程控制系统。本文着重讨论了远程控制的实施方案 ,包括天线当前的性能测试、如何安全地做到远程通信、前端控制 (即现场控制 )等问题 ,把TCP/IP协议族原理和Client/Server原理与模糊逻辑控制思想相结合 ,对 1 0m口径天线实施自动控制 ,并开发了用于现场控制、远程控制的网络控制软件。     

Disturbance compensating control of orbit radially aligned two-craft Coulomb formation

This paper investigates the orbit radial stabilization of a two-craft virtual Coulomb structure about circular orbits and at Earth–Moon libration points. A generic Lyapunov feedback controller is designed for asymptotically stabilizing an orbit radial configuration about circular orbits and collinear libration points. The new feedback controller at the libration points is provided as a generic control law in which circular Earth orbit control form a special case. This control law can withstand differential solar perturbation effects on the two-craft formation. Electrostatic Coulomb forces acting in the longitudinal direction control the relative distance between the two satellites and inertial electric propulsion thrusting acting in the transverse directions control the in-plane and out-of-plane attitude motions. The electrostatic virtual tether between the two craft is capable of both tensile and compressive forces. Using the Lyapunov’s second method the feedback control law guarantees closed loop stability. Numerical simulations using the non-linear control law are presented for circular orbits and at an Earth–Moon collinear libration point.     

On chaos control of nonlinear fractional chaotic systems via a neural collocation optimization scheme and some applications

In this paper, we study chaos control of a class of fractional-order chaotic systems where the dynamic control system depends on the Caputo fractional derivatives. We first propose an infinite horizon optimal control problem related to the given fractional chaotic system. With the help of an approximation, we replace the Caputo derivative to integer order derivative. We then convert the obtained infinite horizon optimal control problem into an equivalent finite horizon one. Based on the Pontryagin minimum principle (PMP) for optimal control problems and by constructing an error function, we define an unconstrained minimization problem. In the optimization problem, we use trial solutions for state, costate and control functions where these trial solutions are constructed by using a two-layered perceptron neural network. A learning procedure of the proposed neural network with convergence properties are also given. Some numerical results are introduced to explain our main results. Three applicable examples on chaos control of Malkus waterwheel, finance fractional chaotic models and fractional-order Geomagnetic Field models are finally considered.     

Station-keeping for a translunar communication station

A translunar communication station is to be kept close to a nominal unstable periodic ‘Halo’ orbit, visible at all times from Earth. The analytically computed nominal orbit is not perfect, requiring an average control acceleration of about 10^?6 g's for tight control. An adjustable quadratic combination of position deviation and control acceleration is minimized to provide an (adjustable) control law with period feedback gains and a periodic bias. The average control acceleration can be reduced to less than 10^?8 g's with an error settling time of less than 21/2 months. The resulting limiting motion provides, in turn, an improved nominal, permitting the same low control cost with much tighter control, corresponding to settling times of the order of one day.     

Artificial Martian frozen orbits and Sun-Synchronous orbits using continuous low-thrust control

This paper analyses three types of artificial orbits around Mars pushed by continuous low-thrust control: artificial frozen orbits, artificial Sun-Synchronous orbits and artificial Sun-Synchronous frozen orbits. These artificial orbits have similar characteristics to natural frozen orbits and Sun-Synchronous orbits, and their orbital parameters can be selected arbitrarily by using continuous low-thrust control. One control strategy to achieve the artificial frozen orbit is using both the transverse and radial continuous low-thrust control, and another to achieve the artificial Sun-Synchronous orbit is using the normal continuous low-thrust control. These continuous low-thrust control strategies consider J ₂, J ₃, and J ₄ perturbations of Mars. It is proved that both control strategies can minimize characteristic velocity. Relevant formulas are derived, and numerical results are presented. Given the same initial orbital parameters, the control acceleration and characteristic velocity taking into account J ₂, J ₃, and J ₄ perturbations are similar to those taking into account J ₂ perturbations for both Mars and the Earth. The control thrust of the orbit around Mars is smaller than that around the Earth. The magnitude of the control acceleration of ASFOM-4 (named as Artificial Sun-Synchronous Frozen Orbit Method 4) is the lowest among these strategies and the characteristic velocity within one orbital period is only 0.5219 m/s for the artificial Sun-Synchronous frozen orbit around Mars. It is evident that the relationship among the control thrusts and the primary orbital parameters of Martian artificial orbits is always similar to that of the Earth. Simulation shows that the control scheme extends the orbital parameters’ selection range of three types of orbits around Mars, compared with the natural frozen orbit and Sun-Synchronous orbit.     

25m射电望远镜自动换馈系统模糊控制策略的软硬件实现

乌鲁木齐天文站25m射电望远镜的换馈系统是基于精确数学模型和传统控制策略实现的自动控制系统,由于设备老和更改,系统不能正常工作。随着计算机软硬件技术迅速发展和模糊理论的提出完善,在一些特定的环境下,模糊控制策略实现的控制系统取得非常好的效果。自动换馈系统的运行环境比较封闭,比较容易获得控制经验,因此选择基于PC硬件和Windows2000/XP平台,采用模糊控制策略来实现对馈源的更换。     

卫星激光测距的电控系统设计与实现

给出的卫星激光测距的二轴系统实现了通过软件控制望远镜coude光路调整、接收系统SPAD和APD的自动切换、视场光阑大小的自动调节、以及发射光束指向的精确控制。该系统是基于MPC07运动控制卡,通过人机交互界面进行实时控制,旨在实现不同功能的调节,提高卫星激光测距的自动化程度。详细介绍了该系统的硬件组成、技术指标及软件工作方式。     

Ensuring dynamic stability of the orbital structure of the Arktika-M space system

The control of the orbital structure of the satellite constellation (SC) of continuous service with spacecraft in highly elliptical orbits of the Molniya type is considered. For ensuring the SC dynamic stability, it is proposed to use passive, active, and combined approaches to the SC orbital structure control. A statement of the problem to ensur e dynamic stability is given and results of its solution for a particular variant of the orbital construction of the Arktika-M space system are presented for the passive control approach. The proposed orbital structure control is based on minimizing the evolution-induced space-time deformation of the orbital structure by means of differentiated selection of initial parameters of orbits at the stages of the SC deployment and replenishment and by means of control of the spacecraft’s ground track at the SC operation stage. Using this control method is especially important with long active life spans of spacecraft and limitations on propellant margins for orbit correction.