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Fuzzy Optimum Model of Semi-Structural Decision for Lectotype Optimization of Offshore Platforms 总被引：8，自引：0，他引：8
In the process of concept design of offshore platforms, it is necessary to select the best from feasible alternatives through comparison and filter. The criterion set, used to evaluate and select the satisfying alternative, consists of many qualitative and quantitative factors. Therefore, the selection is a problem of multicriteria and semi- structural decision- making. Different from traditional methods in semi- structural decision- making, a new framework and methodology is presented in this paper for evaluation of offshore platform alternatives. First, the criterion set is established for the evaluation of alternatives. Next, the approach is studied to construct the relative membership degree matrix, in which both qualitative and quantitative factors are consistent with the uniform calculating standard. And then a new weight-assessing method is developed for calculation of the weights based on the relative membership degree matrix. Finally, a multi-hierarchy fuzzy optimum model is adopted to select t 相似文献
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LIU Guoping OUYANG Ziyuan LI Chunlai LIU Jianfeng National Astronomical Observatories Chinese Academy of Sciences Beijing Peking University of Aeronautics Astronautics Beijing 《《地质学报》英文版》2004,78(5):1104-1108
The data acquisition stations and the data processing center of the Science and Application Center for Lunar and Deep-space Exploration (SACLuDE) are located at different geographical sites. They respectively have their own local networks and interconnect with each other through access to the core data network. This paper describes the clock drift in the computer and other networked devices building up the infrastructure of the above local networks. The network time variance of the stochastic model is also estimated. The poor precision of network synchronization will bring about potential hazards to the network operation and application running in the networks, which is clarified in the present paper. At the end of the paper, a cost-effective and feasible solution is proposed based on the Global Position System (GPS) and the Network Time Protocol (NTP). 相似文献
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Srinivas N. Mohan Ph.D. Candidate Dept. of Aeronautics Astronautics John V. Lange Benjamin O. Lange 《Celestial Mechanics and Dynamical Astronomy》1972,5(2):157-173
Interaction between orbital motion and attitude libration dynamics of an arbitrary rigid body moving in a central Newtonian field is considered to second order. Advantage is taken of the decoupling between inplane-pitch and roll-yaw out-of-plane motion to restrict the motion to the orbital plane by an appropriate choice ofinitial conditions. An averaged solution to the nonlinear inplane-pitch equations whose accuracy is determined by ignoring terms of order {·G32/a
2, 2,2,G32/a
2} and higher is presented. The results show that the near-resonant motion is characterized by a periodic interchange of energy between the attitude and orbital motion.Associate Professor, Department of Aeronautics and Astronautics. 相似文献
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北斗卫星导航系统的信号体制与GPS近似且占用相同的频段,不可避免地带来兼容性问题。从理论上分析兼容性评估的重要参数:频谱分离系数、码跟踪谱灵敏度和等效载噪比衰减,阐述伪随机码码长、导航数据速率和码片速率对兼容性计算的影响,在综合考虑信号兼容评估的运算速度和准确性的基础上,提出改进的GNSS兼容性评估模型。以此兼容性评估模型对北斗卫星导航系统和GPS所有频段进行仿真,仿真分析中考虑北斗卫星导航系统和GPS的具体频率分配、信号体制、发射功率、发射带宽、卫星天线增益、仰角、多普勒偏移、信号在空间传播的衰耗以及接收机参数。通过仿真可以看出,当北斗卫星导航系统满星座运行时,GPS对北斗系统的干扰将大于北斗系统对GPS的干扰。 相似文献
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XING Lida WU Jianghao LU Yi L Junchang JI Qiang Institute of Geology Chinese Academy of Geological Sciences Beijing China School of Transportation Science Engineering Beijing University of Aeronautics Astronautics Beijing China 《《地质学报》英文版》2009,83(1)
The Nyctosaurus specimen KJ1 was reconstructed under the hypothesis that there is a membrane attached to the crest;the so-called headsail crest.The aerodynamic forces and moment acting on the headsail crest were analyzed.It was shown that KJ1 might adjust the angle of the headsail crest relative to the air current as one way to generate thrust (one of the aerodynamic forces,used to overcome body drag in forward flight) and that the magnitude of the thrust and moment could vary with the gesture angle and ... 相似文献
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