基于实时视景仿真技术的海上航标监管系统

海上航标系统是海上交通安全保障体系的重要组成部分。结合上海海事局厦门航标处的航标日常管理与实时监控的实际业务需求,开展了利用实时视景仿真技术与电子海图相结合构建海上航标监管系统的应用研究和系统实现等工作。该系统的实现,有利于航标设置方案的审定与选择,有利于监控者对现场环境的把握和应急决策。     

基于ANN星识别算法的仿真平台

星敏感器是一种高精确度的姿态测量仪器，它通过对观测到的星点进行识别来计算姿态。为了能够较好地测试和验证星识别系统的性能，设计了一个基于ANN算法的星识别仿真平台。通过对该星识别仿真平台性能的测试，表明该仿真平台能够方便，实时地测试星识别算法的性能与正确性，因此说它是一种具有较好实用价值的星识别仿真平台。     

我国高速铁路速度目标值问题的研究

196 4年日本建成东海道干线时速 2 0 0 km/h的高速客运铁路 ,揭开了世界高速铁路发展的序幕。由于高速技术日趋成熟和它自身所具有的技术经济特征 ,适应了各国经济、社会发展的需要 ,世界各国竞相提高速度、修建高速客运铁路 ,至今已有 10个国家 (日本、法国、英国、美国、意大利、西班牙、荷兰、俄罗斯等 )建成时速 2 0 0 km/h以上的高速铁路。高速铁路的修建和发展标志着世界铁路已进入了向高速发展的新时代。本论文不涉及对高速铁路系统模式优劣的比选 ,仅就对已报国家审批的高中速共线方案的高速铁路中的有关问题进行研究和探讨。本文提出了我国发展高速铁路是当务之急 ,讨论了高速铁路目标值的确定 ,对于高中速共线运行方案下的有关部分参数选取 ,提出了优化方法 ,以期为高速铁路规划和建设作参考 ,为深化研究提供基础条件。     

京秦线提速路涵过渡段动力仿真与试验对比

结合京秦线提速改造工程进行了列车 路基动力仿真计算。在不同速度条件下,通过对路涵过渡段加固前后状态下机车车辆运行安全舒适性指标、轨道及路基主要动力性能指标的分析计算,对京秦既有线路涵过渡段提速到200km/h的适应性及加固方案的可行性提出了相应评价意见与建议,并与随后的实车试验进行了对比。试验测试结果验证了仿真分析的可靠性。     

Experimental ivnestigation on flow fields of viscous fluid around two-dimensional wings and comparison with computational results

To examine the flow field of a viscous fluid around the trailing edge of a wing with respect to the Kutta condition or the Joukowski hypothesis, an experimental investigation into the velocity fields around two-dimensional (2D) wings NACA0012 and NACA4412 was carried out using an X-type hot-wire anemometer in a wind tunnel and the method of colored milk injection in a circulating water channel. The results of these investigations revealed that the flow of a viscous fluid at the trailing edge of a 2D wing is tangential to the face on the pressure side, and that the flow is very slow or reversed on the suction side due to separation when the angle of attack is greater than 7.5°. By flow visualization, a Kármán vortex street was found in the wake of both wings (NACA0012 and NACA4412) when the angle of attack was 5°. These results show that the ordinary Kutta condition with respect to the direction of outflow at the trailing edge is not necessarily satisfied in a viscous fluid, but the Kutta condition with respect to the pressure at the trailing edge is satisfied as usual. Numerical results, which have been obtained as the solution of Reynolds-averaged Navier-Stokes equations, show good agreement with above-mentioned experimental results. Therefore, CFD (Computational Fluid Dynamics) simulation has proved to be very effective for studying steady viscous flow around the trailing edge of a 2D wing.     

Development of Green-Naghdi models with a wave-absorbing beach for nonlinear, irregular wave propagation

Two-dimensional and three-dimensional Green-Naghdi (GN) models equipped with a numerical wave-absorbing beach have been developed to simulate nonlinear, regular, and irregular wave propagation. The numerical beach is introduced near the downstream boundary to absorb outgoing waves. An appropriate amount of numerical damping and an appropriate length of numerical beach are investigated using numerical experiments. The results show that the GN models with a numerical beach work very well in simulating wave propagation in water in a small computational domain.     

多值非线性系统的自适应控制

提出了带有多值非线性环节的线性离散系统的自适应控制算法，仿真实验的结果表明：该算法简单易行具有明显的优点，跟踪误差比采用一般的自适应控制算法时要小得多，且能保证闭环系统大范围近收敛。     

Dynamic Simulation of a Smart Crank and Slider Mechanism

In this paper, a smart crank and slider mechanism is analyzed mostly from a dynamic view. By means of dynamic explicit finite element method, 3D nonlinear structure is simulated. It is proved that the mechanism can effectively accomplish smart movement prescribed. And in order to ensure reciprocal movement with higher frequency, measures should be taken to avoid over heating of parts. Compared with internal energy, kinetic energy of total rigid body is dominating, and Y direction equivalent rigid velocity is much higher than X direction velocity. Equivalent rigid velocity of all parts is consistent with respective movement condition. For both energy and velocity, slider effect is dominating. Three direction equivalent inertia force oscillates. Force amplitude in Y -direction is comparitively the greatest.     

滑行艇和翼滑艇在正横规则波中的线性横摇仿真研究

建立滑行艇和翼滑艇在正横规则波中的二阶线性横摇运动微分方程,并利用前苏联中央流体动力中心ЦАГИ法得到艇体阻力,利用仿真工具Matlab/Simulink建立滑行艇和翼滑艇的横摇运动、阻力及推进系统的综合仿真模型,仿真计算结果表明建立的横摇运动微分方程较为合理,并验证具有前置V型割划式水翼的翼滑艇其横摇自稳特性要比同等吨位的滑行艇优良许多。     

同步发电机参数辨识的相关方法探讨

随着电网安全及稳定运行问题的重要性日益突出,基于获得准确的系统模型和参数辨识方法,优化同步发电机相关参数将是十分有意义的。本文针对当今几种比较典型的参数辨识方法做了系统的介绍,通过比较得出何种方法对于同步电机的参数辨识是最适合的。