基于单片机TC275的无人物流车控制器设计

基于英飞凌单片机TC275设计了无人物流车的控制器.TC275通过解析惯性导航仪得到自车信息,并且接收来自计算平台NVIDIA JetsonTX2的路径规划决策信息.在应用层建立了基于模型预测控制算法的路径跟踪模型并生成代码,在底层设计了串口驱动、GTM驱动、ADC驱动以及CAN通信,控制无人物流车的驱动电机和转向舵机...     

基于模型预测控制无人驾驶车辆避障轨迹跟踪器设计

针对无人驾驶车辆的轨迹跟踪和避障问题,基于模型预测控制算法设计了避障轨迹跟踪控制器,实现避障和轨迹跟踪功能。在不同车速下采用Matlab和CarSim进行联合仿真试验,结果表明:设计的控制器控制性能和稳定性良好,能满足无人驾驶车辆的避障和轨迹跟踪需求。     

依据管制员工作负荷的扇区优化方法

为了保证飞行的安全性,提高空域容量,在提出了管制员工作负荷的统计方法和建立空域拓扑结构数学模型的基础上,以各扇区工作负荷均衡为优化原则,利用模拟退火随机优化算法对扇区最优化问题进行求解,并使优化的新解满足空域划分的优先搜索、扇区连续性和扇区数最少原则。对厦门管制区的扇区最优划分实例分析表明,3个扇区之间最大工作负荷之差为4．1s,小于规定的终止条件17．5S,验证了扇区优化方法是可行的。     

基于模型预测控制的智能车横纵向控制器设计

针对智能车横纵向控制中路径跟踪精度、行驶稳定性以及乘坐舒适性等问题,提出了基于模型预测控制(MPC)的横纵向综合控制方法.速度规则系统根据参考路径曲率与车辆跟踪位移误差计算出期望速度曲线,速度跟踪控制采用分层式控制器,上层控制器利用MPC算法计算期望加速度,下层控制器利用车辆逆纵向动力学模型对车辆的驱动和制动进行协调控...     

分布式MAS 在飞行冲突解脱中的应用研究

在自由飞行的环境下,为解决飞行冲突探测与解脱（conflict detection and resolution,CDR）问题,提出一种基于高度层、航向和速度调配的综合解脱方法,并将多 agent 系统(multi-agent system, MAS) 的分布式技术与启发式算法相结合,进行问题求解. 首先设计了分布式MAS框架结构,然后建立了飞行冲突探测模型,高度层调配模型及航向、速度调配模型,最后,综合运用了基于合同网协议的分布式算法和自适应遗传算法进行问题求解.仿真实验表明,所设计的MAS框架是可行的,同时分布式算法和自适应遗传算法的综合应用能很快找到基于高度层、航向和速度分配的近似最优解,为CDR问题提供了新的解决思路.     

直升机贴地飞行操纵系统中的光传点-点链路

为了实现多种传输速度和数据格式信号的光纤传输，开发了基于串口通讯的点-点链路光传操纵技术．以直升机飞行控制系统为背景，构建了飞行控制系统的地面光传半物理平台，建立了显模型计算机与飞行控制计算机之间、飞行控制计算机与实物舵机之间的通信．光/电传试验仿真表明，所开发的显模型跟踪光传系统LED（发光二极管）的中心波长为820nm，最大传输距离400m，远大于实际需要的光纤长度；飞行状态能准确地跟踪显模型输出，跟踪度不小于90．11％．     

Weekly Fleet Assignment Model and Algorithm

A 0-1 integer programming model for weekly fleet assignment was put forward based on linear network and weekly flight scheduling in China. In this model, the objective function is to maximize the total profit of fleet assignment, subject to the constraints of coverage, aircraft flow balance, fleet size, aircraft availability, aircraft usage, flight restriction, aircraft seat capacity, and stopover. Then the branch-and-bound algorithm based on special ordered set was applied to solve the model. At last, a real-world case study on an airline with 5 fleets, 48 aircrafts and 1786 flight legs indicated that the profit increase was $1591276 one week and the running time was no more than 4 min, which shows that the model and algorithm are fairly good for domestic airline.     

着陆阶段航空器航迹检测与风险识别方法

进近着陆是整个飞行过程中最易发生危险的阶段.目前着陆阶段的风险识别 只能依靠塔台管制员的目视观察.在飞行员技术不熟练、起降频繁的通用航空飞行训练 中,目视观察很难准确掌握情况,也因此蕴含了巨大的安全风险.利用视频监视航空器着 陆行为,同时提出了一种适合复杂背景下小目标分割算法,从视频中提取航空器着陆航 迹;并以此为基础进一步识别降落过程中的运行风险.通过对多组不同角度的视频监视数 据验证,该算法可在复杂背景下实现航空器着陆航迹的跟踪、落地时刻的判断及危险滑 行航迹的准确识别,对于保障飞行安全具有重要的现实意义.     

基于等值线搜索带的地磁匹配算法

针对TERCOM算法在地磁匹配应用中存在的不足,提出了基于等值线搜索带的改进匹配算法,将地磁基准图上的匹配搜索区域缩小到航迹起始点地磁测量值对应的地磁场等值线附近区域,从而减少匹配搜索时间和计算量.仿真实验结果表明,该算法在保证匹配精度的前提下,能够有效降低匹配计算时间,提高匹配算法的实时性.     

A Hybrid Heuristics for Irregular Flight Recovery

Adverse weather conditions, congestion at airports, and mechanical failures often disrupt regular flight schedules. The irregular flight recovery problem aims to recover these schedules through reassignments of flights and cancellations. In this article, we develop the classic resource assignment model for the irregular flight recovery problem, and a new hybrid heuristic procedure based on greedy random adaptive search procedure (GRASP) and simulated annealing algorithm is presented to solve this problem. As compared with the original GRASP method, the proposed algorithm demonstrates quite a high global optimization capability. Computational experiments on large-scale problems show that the proposed procedure is able to generate feasible revised flight schedules of good quality in less than five seconds.     

离场航迹降噪优化设计的多目标智能方法

为满足新一代空管系统中离场航迹优化设计时降低噪声影响和减少飞行成本的需要,进行了离场航迹的多目标优化设计方法研究.结合飞行动力学和运动学模型,建立了符合民航飞机离场飞行阶段特征的航迹分段模型,提出了应用状态矩阵和控制矩阵准确表示航迹的数学方法.基于模糊理论建立航迹噪声影响、飞行成本和空中导航约束的满意度评价函数,提出了3种启发式搜索规则和动态领域搜索方法来改进模拟退火算法.仿真结果表明,在绕飞限制空域的前提下,降噪和减少飞行成本的目标无法同时达到最优;离场航迹多目标优化后的总体满意度比仅考虑降噪时提高了4.3%.      

遗传算法用于控制器参数的满意优化

对于控制器参数的多指标优化问题，提出了一种新型优化设计方法。通过分别设计的各个性能指标的满意度函数，反映出各性能指标对控制系统的具体要求；并用综合满意度函数的设计，反映出对控制目标的综合要求。由此给出了一种优化模型。应用遗传算法自动搜索，实现控制器参烽的优化。仿真实验效果良好，表明了本文方法的灵活实用性。     

基于延误传播的飞机排班一体化鲁棒优化模型

为了减少航班延误对航班运行计划的影响,在分析航班延误传播特性及其分布的基础上,以总波及延误时间最少和航空公司运营成本最小为优化目标,建立了双目标飞机排班一体化网络流鲁棒优化模型.将该模型应用于国内某航空公司的实际运营数据进行实例分析,利用列生成和分枝定价法求解,结果表明:用本文模型优化后的航班计划使航班延误传播减少了41%;运营总成本比航空公司实际成本减少了11.33%,比没有考虑鲁棒性的飞机排班一体化模型的成本减少了9.93%.      

LQR-GA Controller for Articulated Dump Truck Path Tracking System

This paper designs a novel controller to improve the path-tracking performance of articulated dump truck(ADT). By combining linear quadratic regulator(LQR) with genetic algorithm(GA), the designed controller is used to control linear and angular velocities on the midpoint of the front frame. The novel controller based on the error dynamics model is eventually realized to track the path high-precisely with constant speed. The results of simulation and experiment show that the LQR-GA controller has a better tracking performance than the existing methods under a low speed of 3 m/s. In this paper, kinematics model and simulation control models based on co-simulation of ADAMS and Matlab/Simulink are established to verify the proposed strategy. In addition, a real vehicle experiment is designed to further more correctness of the conclusion. With the proposed controller and considering the steering model in the simulation, the control performance is improved and matches the actual situation better. The research results contribute to the development of automation of ADT.     

Robust intelligent control design for marine diesel engine

This work deals with the nonlinear control of a marine diesel engine by use of a robust intelligent control strategy based on cerebellar model articulation controller （CMAC）. A mathematical model of diesel engine propulsion system is presented. In order to increase the accuracy of dynamical speed, the mathematical model of engagement process based on the law of energy conservation is proposed. Then, a robust cerebellar model articulation controller is proposed for uncertain nonlinear systems. The concept of active disturbance rejection control （ADRC） is adopted so that the proposed controller has more robustness against uncertainties. Finally, the proposed controller is applied to engine speed control system. Both the model of the diesel engine propulsion system and of the control law are validated by a virtual detailed simulation environment. The prediction capability of the model and the control efficiency are clearly shown.     

一种新的CMAC自学习控制器

本文通过分析ＣＭＡＣ神经网络的学习机制和连续搅拌反应釜的结构,提出了一种自动选择学习率的ＣＭＡＣ自学习控制方法。给出了自学习控制器的结构和算法。并以连续搅拌反应釜模型为对象进行了仿真研究。这种网络每次学习少量参数,算法简单。仿真结果表明所提出的控制器优于传统的ＰＩＤ控制器。     

Application of Nonlinear Predictive Control Based on RBF Network Predictive Model in MCFC Plant

This paper described a nonlinear model predictive controller for regulating a molten carbonate fuel cell (MCFC). A detailed mechanism model of output voltage of a MCFC was presented at first. However, this model was too complicated to be used in a control system. Consequently, an off line radial basis function (RBF) network was introduced to build a nonlinear predictive model. And then, the optimal control sequences were obtained by applying golden mean method. The models and controller have been realized in the MATLAB environment. Simulation results indicate the proposed algorithm exhibits satisfying control effect even when the current densities vary largely.     

带有UKBF的船舶动力定位预测控制器设计

为了精准设计水面船舶动力定位控制系统,将无迹卡尔曼布西滤波与非切换解析模型预测控制方法相结合提出一种预测控制器的设计方法.采用无迹卡尔曼布西滤波算法解决非线性连续系统的滤波问题,获取船舶运动状态的估计值;结合相对阶概念,根据船舶运动非线性模型,应用非切换解析模型预测控制方法设计动力定位非线性控制器,使船舶保持在指定位置.研究结果表明:设计控制器的输出较为平滑,有利于减少推进器磨损;设计控制器使船舶北向位置调节时间小于40 s,超调量小于5%,东向位置调节时间小于60 s,超调量小于5%,艏向角度的最大偏移量小于1.5°,令船舶快速到达了指定位置.      

一类非线性系统的神经网络内模优化控制

研究一类可用Ｈａｍｍｅｒｓｔｅｉｎ模型描述的ＭＩＳＯ非线性系统的优化控制方法，提出一种基于前向神经网络的Ｈａｍｍｅｒｓｔｅｎ模型，以描述ＭＩＳＯ非线性对象并给出具有内模结构的优化控制器设计方法，从而实现了在稳态优化与动态优化双重指标下的设定值闭环优化控制。针对汽油管道调合系统进行的仿真实验，验证了该方法的有效性。     

Hierarchical control strategy of trajectory tracking for intelligent vehicle

In order to track the desired trajectory for intelligent vehicle, a new hierarchical control strategy is presented. The control structure consists of two layers. The high-level controller adopts the model predictive control (MPC) to calculate the steering angle tracking the desired yaw angle and the lateral position. The low-level controller is designed as a gain-scheduling controller based on linear matrix inequalities. The desired longitudinal velocity and the yaw rate are tracked by the adjustment of each wheel torque. The simulation results via the high-fidelity vehicle dynamics simulation software veDYNA show that the proposed strategy has a good tracking performance and can guarantee the yaw stability of intelligent vehicle.