禁飞区无人机预警算法研究

针对大量在空中无秩序飞行的无人机有可能会闯入飞机场等禁飞区的情况,为了避免发生空中交通安全事故,提出了一种无人机禁飞区预警算法。首先,该算法经过坐标变换将描述无人机位置点的GPS坐标转换成对应的平面坐标;接着,采用改进的最小二乘曲线拟合算法预测出无人机的飞行轨迹;然后,通过计算预测的飞行轨迹曲线在当前点的切线是否会与描述禁飞区的电子围栏相交,来判断无人机是否会进入禁飞区。同时,所有的无人机都会安装上飞行数据记录模块,来实时地为该算法提供无人机的飞行状态信息。最后,通过MATLAB仿真实验验证了该预警算法的可行性和有效性,表明该算法可以对禁飞区周围的无人机进行预警。     

重力不同引起的载人月球车操纵差异分析

为分析月球与地球重力差异对驾驶员所带来的操纵影响,推导了载人月球车操纵动力学方程.基于径向基神经网络和间接逆模型的训练方法,建立以行驶轨迹为输入、驾驶员操纵转角为输出的载人月球车操纵动力学逆系统.采用两种不同类型的间接对比形式,包括地球重力条件下重复月面行驶的轨迹路线和月球重力条件下重复地面行驶的轨迹路线.将正弦函数和斜坡阶越函数作为驾驶员操纵输入,获得月球或地球重力条件下的行驶轨迹,并利用逆系统求解得到不同重力条件下行驶相同轨迹时驾驶员的操纵转角.结果表明,驾驶员在月球重力条件下需要做出更大的操纵转向角度、更快的操纵转向速度、更高的操纵转向变换频率,并且在月球重力条件下更不容易重复地球重力条件下的相同行驶轨迹.这说明载人月球车在月球重力条件下的操纵性能较差.     

基于ArcGisServer的高速公路数据校验系统设计与研究

介绍了Arc Gis Server的体系结构和开发方法,系统实现了地图图层的控制与显示、路径和费额查询与校对、历史行进道路的回放、空间数据的查询、最短路径和最小收费额显示等关键模块。为优化路况、提高公路通行率、减少人为干预、降低人工成本提供了技术支撑,并以贵州省高速公路为实际应用背景展示了整个系统的功能。     

智能电网中电动汽车充电的自适应电价控制方法

针对电动汽车的充电提出一种电价控制策略。聚合管理者集中管理电动汽车的电池,并且考虑用电高峰时电网的电能供给有限,通过电价控制调整充电的需求量。采用自适应动态规划,通过在线网络训练,得到最优的电价策略。仿真结果表明,该自适应电价控制方法能够通过学习电动汽车的移动性和充电过程,从而调整实际充电需求量至期望水平,保证智能电网的稳定运行。     

Adaptive key SURF feature extraction and application in unmanned vehicle dynamic object recognition

A new method based on adaptive Hessian matrix threshold of finding key SRUF( speeded up robust features) features is proposed and is applied to an unmanned vehicle for its dynamic object recognition and guided navigation. First,the object recognition algorithm based on SURF feature matching for unmanned vehicle guided navigation is introduced. Then,the standard local invariant feature extraction algorithm SRUF is analyzed,the Hessian Metrix is especially discussed,and a method of adaptive Hessian threshold is proposed which is based on correct matching point pairs threshold feedback under a close loop frame. At last,different dynamic object recognition experiments under different weather light conditions are discussed. The experimental result shows that the key SURF feature abstract algorithm and the dynamic object recognition method can be used for unmanned vehicle systems.     

Rigid-Flexible Coupling Dynamic Analysis of Sub-Launched Vehicle During the Vertical Tube-Exit Stage

During the launching stage,hydrodynamic pressure and adapters’ reaction loads can influence the vehicle’s rigid motion as well as cause its structural vibration,which is a typical rigid-flexible coupling dynamic problem. This paper presents a 2-D rigid-flexible coupling model to calculate the vehicle’s dynamic responses in that period.The vehicle was equivalent to a flexure beam with axial deformation. Hybrid coordinate and modal superposition methods were used to describe its large rigid displacement and small deformation. By the second Lagrange equation,the vehicle centroid’s displacements,rotational angle and modal coordinates were chosen as generalized coordinates and then the vehicle ’s rigid-flexible coupling dynamic equations were obtained. By numerical simulation,the results of vehicle’s motion parameters and transverse internal loads were acquired.The calculation results showed that differences of the vehicle’s motion parameters between the rigid-flexible coupling model and the rigid body assumption are noticeable and the peak magnitude of the vehicle’s transverse internal loads in the rigid-flexible coupling model is higher remarkably than that in the rigid body assumption.     

Research and Application of Dynamic Equation for Full Frontal Impact

Full frontal impact theory needs researching and exploring to satisfy the primary safety design of occupant restraint system,avoiding the increasingly "engineering"trend in order to develop and design safety vehicle. After occupant restraint system is simulated by using linear elastic stiffness k,the occupant-vehicle frontal rigid barrier impact model is established. Dynamic equation of dummy chest coupling vehicle is built for full frontal impact based on ordinary vehicle deceleration by Hooke law,and the equation is solved by comparing coefficient and satisfying boundary qualifications. While relative vehicle characteristic parameters are kept unchanging,the actual vehicle deceleration is fitted to the simplified equivalent square wave( ESW),tipped equivalent square wave( TESW) and equivalent dual trapezoids wave( EDTW). Phase angle  and amplitude A of dynamic equations based on ESW,TESW and EDTW are calculated and deduced. The results show that: the dynamic equation of dummy chest coupling vehicle can be well utilized to instruct the primary safety design of full frontal impact for objective vehicle to satisfy chest deceleration demands and the equation based on TESW is best for this design.     

电动汽车跨区域充换电计量计费清分结算研究

为确保电动汽车跨区域充换电顺利完成电费结算,研究了跨区域充换电的交易流程,并提出一种成本清分和收入清分的方法,并建立了运营商运营成本模型和客户支付充换电的费用单价模型.在此基础上,设计开发了一套清分结算系统,并对上述两个模型的实用性加以论证,为实施跨区域充换电提供参考.     

基于AVR微处理器的钢坯保温车电气系统

为钢坯运输车设计的专用保温罩,其可靠、高效工作有赖于优异的电气控制系统。采用ATMEL公司AVR微处理器为核心,并设计相关接口电路、驱动电路,最后制作出PCB控制板。该控制板能够实现对保温罩的顺序控制、延时控制及故障报警等功能。系统设有用于紧急情况的强制按钮。     

An optimization model of UAV route planning for road segment surveillance

Unmanned aerial vehicle （UAV） was introduced to take road segment traffic surveillance. Considering the limited UAV maximum flight distance, UAV route planning problem was studied. First, a multi-objective optimization model of planning UAV route for road segment surveillance was proposed, which aimed to minimize UAV cruise distance and minimize the number of UAVs used. Then, an evolutionary algorithm based on Pareto optimality technique was proposed to solve multi-objective UAV route planning problem. At last, a UAV flight experiment was conducted to test UAV route planning effect, and a case with three scenarios was studied to analyze the impact of different road segment lengths on UAV route planning. The case results show that the optimized cruise distance and the number of UAVs used decrease by an average of 38.43% and 33.33%, respectively. Additionally, shortening or extending the length of road segments has different impacts on UAV route planning.