Relative positioning of multiple moving platforms using GPS

To obtain subdecimeter level accuracy in relative kinematic positioning, the use of double differenced GPS carrier phase measurement with carrier phase ambiguities fixed to their correct integer values must be adopted. If multiple platforms are available in the configuration, the redundancy provided by the multiplicity of platforms can speed up the time to integer ambiguity fixing while at the same time improve the reliability of the solution. An approach to effectively construct ambiguity constraints through the multiplicity of platforms is presented herein. The use of these ambiguity constraints to position multiple moving platforms with respect to each other is then discussed. A series of simulations and field tests are designed and conducted to investigate the effects of different system parameters on this approach, with a configuration of up to 10 moving platforms. The test results show that the use of ambiguity constraints can improve the time to integer ambiguity fixing by up to 67%, relative to the case when no constraints are used. In addition, the use of ambiguity constraints is found to enhance the ability of the multiple platform system to detect wrong ambiguity fixes.     

Optimization of multiple-impulse minimum-time rendezvous with impulse constraints using a hybrid genetic algorithm

The minimum-time multiple-impulse rendezvous with impulse constraints is investigated in this paper. Based on the Clohessy–Wiltshire (C–W) equations, an optimization model including several different kinds of impulse constraints such as the maximum impulse magnitude, the total velocity change magnitude and the time of imposing impulse for multiple-impulse minimum-time rendezvous is established. A generalized inverse matrix solution for linear equation is applied to avoid handling the terminal equality constraints. In order to obtain the global solution efficiently, a hybrid optimizer combining the advantages of a floating-coded genetic algorithm and simplex method is employed. A low-earth orbit multiple-impulse rendezvous problem is used as an example. The influence of the number of impulses, the optimization variables and the constraints on the solution is analyzed, and the different optimization algorithms are compared. Results indicate our proposed model and approach is effective in designing linearized minimum-time rendezvous trajectory with impulse constraints.     

对高频电路原理图绘制问题的探讨

本文结合Protel 99 SE在高频PCB设计中的应用,着重探讨在电路原理图的绘制上需要重点注意的一些特殊问题,并提出解决问题的方法,尽可能地减小对高频PCB设计的影响,提高PCB设计的效率。     

利用热源温度场迭加法诊断持续点热源的强度及位置

可重复使用运载器的防热瓦故障会使航天器的局部结构产牛热源，并在结构中形成温度场。应用热源温度场迭加法的解函数，解得结构温度历程，然后据此温度的变化率趋势判断出热源位置，在此基础上依据多点测最值构造出辨识参数用于热强度识别，通过对一薄壁结构模型算例的计算仿真，证明了本文所提方法的有效性。论文工作为进一步开展热源诊断技术研究，提供了可资工程实践应用的数值算法体系以及有益的数值计算结论。     

Sustained data recording system based on disk array

Most sustained data recording systems in many real-time fields are based on tape equipments. We have developed an innovative sustained data recording system based on disk array which consists of Array Controller Module (ACM), String Controller Module (SCM) and Main Controller Module (MCM). This system has a better performance and higher reliability than the traditional tape recorder and can be used conveniently in many areas of data recording, storing, playback, and remote backup. This novel recording system has been used in radar data recorder for spacecraft orbit tracking and satellite remote sensing data recording successfully.     

现场动平衡技术在生产中的应用

利用美国恩泰克公司提供的DP1500数据采集仪及现场动平衡软件,以实例说明了现场动平衡技术在锅炉引风机、排粉风机、电动机、机泵等转动设备不平衡故障排除中的应用,介绍了不平衡故障的识别方法,揭示出该技术在生产中的实用性、先进性和经济性.     

基于混合灵敏度下H∞控制在三滑块质量矩导弹上的应用

由于质量矩导弹是一个具有非线性和模型不确定性的多变量系统，为了进一步提高控制系统的鲁棒性，对三滑块质量矩导弹进行了鲁棒控制系统的研究。以所建立的质量矩导弹数学模型为基础，通过对模型合理的简化，得到一个耦合的非线性动力学系统，考虑到质量矩导弹的鲁棒性要求和三个滑块的协调控制问题，在混合灵敏度控制的基础上，采用H∞控制理论对导弹进行姿态控制系统的研究，仿真结果验证了这种方法的有效性。     

称重传感器的一种新的滞后补偿方法(英文)

通过对电阻应变式称重传感器在各种加载卸载情况下的滞后特性的分析 ,建立了其相应的数学模型 ,并初步探讨了一种可以通过程序在仪表中对传感器的重要指标—滞后进行补偿从而提高整个传感器的精度的方法。最后 ,对以上方法进行了验证性试验 ,证明了补偿方法的可行性。     

数学教学中培养创造能力的探索

本文结合多年教学实践，对激发学生的创造意识，培养发散思维，运用创造技法等方面进行了探索。     

新一代民用客机自主式数据总线

本文在简要阐述 ARINC 429 和 MIL-STD-1553B 总线应用所受限制的基础上,介绍了90年代美国民航界推出的一种自主式数据总线 ARINc629的设计要点,包括其通信协议。各终端信源数据在总线上的周期传输和非周期传输、信息传输的种类和方法及终端的功能框图,最后给出了此总线在新一代民用机中的应用情况。