月球探测器软着陆最优末制导策略

在制动火箭推力幅值满足连续可变的前提下,研究了月球探测器软着陆末端的垂直下落过程中的控制问题。基于线性系统跟踪控制理论,利用线性系统中的模型参考跟踪控制的方法设计了一种对指定轨迹进行跟踪的制动方案。同时为了满足耗燃最优性和安全性,根据最优化理论,对控制律中的参数进行优化,最终确定系统的控制律。仿真结果表明该设计方法是简单、有效的。     

卫星全景象片的几何校正

本文给出了卫星全景相片的几何校正模型。该模型由三部分组成:1.推导了卫星全景相片的几何校正模型;2.给出了计算卫星姿态运动和卫星轨道运动的计算公式;3.用系统辨识方法估算卫星姿态运动公式。     

Aerodynamic and Acoustic Optimization for Multi-element Airfoils

The paper is to integrate aerodynamic and aero-acoustic optimizatiom design of high lift devices,especially for two-element airfoils with slat.Aerodynamic analysis on flow field utilizes a high-order,high-resolution spatial differential method for large eddy simulation(LES),which can guarantee accuracy and efficiency.The aeroacoustic analysis for noise level is calculated with Ffowcs Williams-Hawkings(FW-H)integration formula.Fidelity of calculation is verified by standard models.Method of streamline-based Euler simulation(MSES)is used to obtain the aerodynamic characters.Based on the confirmation of numerical methods,detailed research has been conducted for the leading edge slat on multi-element airfoils.Various slot parameter influences on noise are analyzed.The results of the slot optimization parameters can be used in multi-element airfoil design.     

计算机辅助质量控制图的应用

在现场利用控制图监控生产过程,调查生产过程的状态,了解工序能力是否适宜,实现了预防为主的思想.如果用手工对控制图进行设计和准则判断非常麻烦,难以在实际生产中推广应用.利用计算机辅助控制图,具有准确、方便、直观和快捷的特点.作者设计和开发了"质量控制模拟系统"软件,该软件适用于操作者在现场对生产状态进行分析和判断,及时预防和控制生产过程,也可作为一种有效的辅助教学软件.      

表面贴装元件手工拆卸和焊接方法

由于表面贴装元件应用日益广泛,要掌握手工拆卸和焊接方法,除了能熟练使用焊接工具外,还要通过大量的实践掌握拆卸和焊接的技巧和方法。     

二维翼型微吸吹气减阻控制新技术数值研究

结合抽吸气转捩控制和微吹气湍流减阻控制的特点,探索了一种新的吸吹气减阻控制技术。使用Fluent求解器,并利用用户自定义函数(UDF)二次开发对其自带的Wilcox转捩模式进行了修正。在此基础上,数值研究了吸吹气控制对翼型阻力性能的影响。结果表明：在一定的吸气量范围内,吸气、吸吹气控制都能使翼型总阻力减小,且在同一雷诺数下,吸气控制能使翼型总阻力减小约3%,而吸吹气联合控制使翼型总阻力减小约16%。由此可见,吸吹气控制技术是一种行之有效的减阻控制技术。     

基于计算机视觉的UAV自主空中加油半物理仿真

设计并实现了一种基于计算机视觉的无人机（UAV,Unmanned Aerial Vehicle）自主空中加油仿真平台,采用点匹配与位姿估计算法对软管式加油锥发光二极管（LED,Light Emitting Diodes）标志进行识别.对大气扰动和尾涡流进行了建模,建立了加油锥模型,并设计了加油锥运动状态预估算法.在此基础上,设计了基于线性二次型调节器（LQR,Linear Quadratic Regulator）的飞行控制律.基于上述技术,在实验室环境下设计开发了基于单目机载摄像机的无人机自主空中加油半物理仿真平台.半物理试验结果表明：所设计的位姿匹配算法和飞行控制律能够满足复杂环境下无人机自主空中加油的性能要求,具有较强的实时性、准确性和鲁棒性.     

真空绝热板的研究进展

综述了真空绝热板(VIP)的超高效绝热性能,介绍了VIP的选材和研究现状,提出了存在问题及对VIP的应用进行了展望.     

Novel intelligent water drops optimization approach to single UCAV smooth trajectory planning

Trajectory planning of unmanned combat aerial vehicle (UCAV) is a rather complicated global optimum problem in UCAV mission planning. Intelligent water drops (IWD) algorithm is newly presented under the inspiration of the dynamic of river systems and the actions that water drops do in the rivers, and it is easy to combine with other methods in optimization. In this paper, we propose an improved IWD optimization algorithm for solving the single UCAV smooth trajectory planning problems in various combating environments. The water drops can act as an agent in searching the optimal UCAV trajectory. The detailed realization procedure for this novel approach is also presented. In order to make the optimized UCAV trajectory more feasible for exact flying, an efficient path smoothing method called the κ-trajectory is adopted for smoothing the single UCAV trajectory. Series experimental comparison results show the proposed IWD optimization algorithm is more effective and feasible in the single UCAV smooth trajectory planning than the basic IWD model.