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国家自然科学基金(51105040)

作品数:9 被引量:149H指数:5
相关作者:龙腾刘莉刘建黄波彭磊更多>>
相关机构:北京理工大学中国空间技术研究院更多>>
发文基金:国家自然科学基金中国航空科学基金教育部重点实验室基金更多>>
相关领域:航空宇航科学技术兵器科学与技术军事理学更多>>

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9 条 记 录,以下是 1-10
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Global Optimization Method Using SLE and Adaptive RBF Based on Fuzzy Clustering被引量:8
2012年
High fidelity analysis models,which are beneficial to improving the design quality,have been more and more widely utilized in the modern engineering design optimization problems.However,the high fidelity analysis models are so computationally expensive that the time required in design optimization is usually unacceptable.In order to improve the efficiency of optimization involving high fidelity analysis models,the optimization efficiency can be upgraded through applying surrogates to approximate the computationally expensive models,which can greately reduce the computation time.An efficient heuristic global optimization method using adaptive radial basis function(RBF) based on fuzzy clustering(ARFC) is proposed.In this method,a novel algorithm of maximin Latin hypercube design using successive local enumeration(SLE) is employed to obtain sample points with good performance in both space-filling and projective uniformity properties,which does a great deal of good to metamodels accuracy.RBF method is adopted for constructing the metamodels,and with the increasing the number of sample points the approximation accuracy of RBF is gradually enhanced.The fuzzy c-means clustering method is applied to identify the reduced attractive regions in the original design space.The numerical benchmark examples are used for validating the performance of ARFC.The results demonstrates that for most application examples the global optima are effectively obtained and comparison with adaptive response surface method(ARSM) proves that the proposed method can intuitively capture promising design regions and can efficiently identify the global or near-global design optimum.This method improves the efficiency and global convergence of the optimization problems,and gives a new optimization strategy for engineering design optimization problems involving computationally expensive models.
ZHU Huaguang LIU Li LONG Teng ZHAO Junfeng
基于约束EGO的对地观测卫星多学科设计优化被引量:5
2018年
在对地观测卫星的总体设计阶段,为提高卫星性能及设计效率,建立以卫星覆盖幅宽和地面分辨率综合指标为目标的数学模型进行优化。考虑轨道、控制、有效载荷、电源以及结构5个分系统的设计变量及约束条件并梳理存在的耦合关系,建立较为详尽的多学科设计优化(Multidisciplinary design optimization,MDO)分析模型,并采用定点迭代法进行多学科分析(Multidisciplinary analysis,MDA)。引入自适应罚函数法处理约束条件,提出一种约束高效全局优化算法(C-EGO)。将C-EGO应用于标准工程测试算例,并与遗传算法(Genetic algorithm,GA)和考虑约束的追峰采样算法(Constraint importance mode pursuing sampling,Ci MPS)代理模优化方法的优化结果进行比较,C-EGO显示出较高的优化效率。最后,将C-EGO应用到对地观测卫星的多学科设计优化问题,与遗传算法(GA)和CiMPS相比,C-EGO能够高效地获取满足复杂约束的最优设计方案。研究结果表明C-EGO求解能够较高效地求解对地观测卫星MDO问题,所建立的卫星多学科设计优化模型与提出的高效的C-EGO方法为卫星MDO研究提供了参考。
龙腾刘建陈余军史人赫袁斌刘莉
关键词:对地观测卫星多学科设计优化代理模型自适应罚函数
Metamodel-based Global Optimization Using Fuzzy Clustering for Design Space Reduction被引量:13
2013年
High fidelity analysis are utilized in modern engineering design optimization problems which involve expensive black-box models.For computation-intensive engineering design problems,efficient global optimization methods must be developed to relieve the computational burden.A new metamodel-based global optimization method using fuzzy clustering for design space reduction(MGO-FCR) is presented.The uniformly distributed initial sample points are generated by Latin hypercube design to construct the radial basis function metamodel,whose accuracy is improved with increasing number of sample points gradually.Fuzzy c-mean method and Gath-Geva clustering method are applied to divide the design space into several small interesting cluster spaces for low and high dimensional problems respectively.Modeling efficiency and accuracy are directly related to the design space,so unconcerned spaces are eliminated by the proposed reduction principle and two pseudo reduction algorithms.The reduction principle is developed to determine whether the current design space should be reduced and which space is eliminated.The first pseudo reduction algorithm improves the speed of clustering,while the second pseudo reduction algorithm ensures the design space to be reduced.Through several numerical benchmark functions,comparative studies with adaptive response surface method,approximated unimodal region elimination method and mode-pursuing sampling are carried out.The optimization results reveal that this method captures the real global optimum for all the numerical benchmark functions.And the number of function evaluations show that the efficiency of this method is favorable especially for high dimensional problems.Based on this global design optimization method,a design optimization of a lifting surface in high speed flow is carried out and this method saves about 10 h compared with genetic algorithms.This method possesses favorable performance on efficiency,robustness and capability of global convergence and gives a new optimization strate
LI YulinLIU LiLONG TengDONG Weili
基于可行方向序列无约束极小化技术外点法的改进协同优化策略被引量:2
2013年
指出准协同优化策略(Collaborative optimization,CO)存在的数值缺陷及其原因。针对系统级优化不满足Kuhn-Tucker条件所导致的计算困难,提出一种基于可行方向序列无约束极小化技术(Feasible direction sequential unconstrainedminimization technology,FD-SUMT)外点法的改进协同优化策略(Enhanced collaborative optimization with FD-SUMT method,ECO-FSM)。在系统级优化中使用FD-SUMT外点法,该方法不依赖Lagrange乘子并且能够将系统级设计变量限定在设计变量可行域内,避免传统SUMT外点法设计变量越界所导致的异常。利用学科间动态不一致信息更新系统级优化中的罚因子以加速学科间的协调。利用测试问题检验ECO-FSM的性能,并与其他的CO进行比较研究。研究结果表明ECO-FSM消除了系统级优化中设计变量越界的现象,收敛性、数值稳定性以及收敛速度得以显著提高。将ECO-FSM用于亚声速喷气式客机总体方案优化设计,优化结果表明ECO-FSM具有工程实用性。
龙腾刘莉彭磊
关键词:多学科设计优化
基于物理规划的无人机多目标航迹规划被引量:3
2014年
无人机航迹规划是典型的多目标优化问题,传统的线性加权和法需反复迭代以确定一组满足工程特性需求的目标权重系数。物理规划方法通过构造偏好函数直接反映规划人员对航迹规划各目标的特性需求,避免了因为反复迭代确定各目标权重系数所导致计算量大的缺陷,因此,将物理规划方法与粒子群优化算法相结合用于无人机多目标航迹规划。仿真实验验证了该航迹规划方法能够获得各目标偏好结构下的折中解。
于成龙刘莉王祝黄波龙腾
关键词:航迹规划多目标无人机
基于粒子群算法的长航时无人机翼型快速优化设计被引量:1
2013年
针对长航时无人机翼型气动性能优化的需求,将CFD分析技术、PSO算法与RBF代理模型方法相结合,提出了一种长航时无人机翼型快速优化设计方法。采用正交基函数描述翼型外形,并通过求解N-S方程获得翼型气动性能。使用标准粒子群优化算法对翼型气动性能进行优化,以提高全局收敛性。考虑到CFD气动分析存在计算耗时的缺点,通过径向基函数代理模型对CFD气动分析模型进行近似,以达到提高优化效率的目的。长航时无人机翼型优化算例研究表明,所提出的快速优化方法在保证优化设计质量的前提下,可以有效地降低优化计算成本,提高优化效率,具有较高的工程实用性。
安林雪龙腾黄波齐竹昌彭磊刘莉
关键词:翼型优化设计粒子群优化算法代理模型长航时无人机
Multi-UAV reconnaissance task allocation for heterogeneous targets using an opposition-based genetic algorithm with double-chromosome encoding被引量:40
2018年
This paper presents a novel multiple Unmanned Aerial Vehicles(UAVs) reconnaissance task allocation model for heterogeneous targets and an effective genetic algorithm to optimize UAVs' task sequence. Heterogeneous targets are classified into point targets, line targets and area targets according to features of target geometry and sensor's field of view. Each UAV is regarded as a Dubins vehicle to consider the kinematic constraints. And the objective of task allocation is to minimize the task execution time and UAVs' total consumptions. Then, multi-UAV reconnaissance task allocation is formulated as an extended Multiple Dubins Travelling Salesmen Problem(MDTSP), where visit paths to the heterogeneous targets must meet specific constraints due to the targets' feature. As a complex combinatorial optimization problem, the dimensions of MDTSP are further increased due to the heterogeneity of targets. To efficiently solve this computationally expensive problem, the Opposition-based Genetic Algorithm using Double-chromosomes Encoding and Multiple Mutation Operators(OGA-DEMMO) is developed to improve the population variety for enhancing the global exploration capability. The simulation results demonstrate that OGADEMMO outperforms the ordinary genetic algorithm, ant colony optimization and random search in terms of optimality of the allocation results, especially for large scale reconnaissance task allocation problems.
Zhu WANGLi LIUTeng LONGYonglu WENa
基于凸优化的无人机三维避障轨迹规划
针对无人机三维避障轨迹规划问题,建立包括非线性动力学、允许控制、状态边界、障碍规避和终端约束的非凸最优控制模型。利用控制与状态离散化方法,将无限维的非凸最优控制问题参数化为有限维的非凸优化问题。在此基础上,引入序列凸化技...
王祝刘莉温永禄龙腾
关键词:无人机凸优化
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改进的Pareto多目标协同优化策略被引量:8
2012年
为了提高标准协同优化的收敛性并扩展其多目标优化能力,将Pareto多目标遗传算法用于协同优化的系统级优化,提出了一种改进的Pareto多目标协同优化策略(enhanced collaborative optimization using Pare-to multi-objective genetic algorithm,ECO-PMGA)。为了保证非劣解集的Pareto最优性与均布性,提出了一种考虑拥挤度的非劣解逐级排序方法。ECO-PMGA采用2-范数形式的学科间一致性约束以提高学科级优化的效率。通过两个典型的优化算例对ECO-PMGA的数值稳定性与搜索Pareto非劣解集的能力进行了检验。研究结果表明,ECO-PMGA的收敛性与数值稳定性得以显著提高,而且ECO-PMGA具有良好的Pareto多目标优化能力。因此,ECO-PMGA在复杂耦合系统的多目标优化设计方面具有较高的实用价值。
龙腾刘莉
关键词:多学科设计优化PARETO最优
基于计算试验设计与代理模型的飞行器近似优化策略探讨被引量:76
2016年
现代飞行器设计优化中广泛应用高精度分析模型以提高设计可信度与综合性能,但是也带来了计算复杂性问题。为了有效缓解计算耗时的问题,基于计算试验设计与代理模型的飞行器近似优化策略成为研究热点。近似优化策略通过构造合理的近似模型引导优化过程快速收敛到最优解,从而达到降低计算成本,缩短设计周期的目的。根据广泛的文献调研,对飞行器近似优化策略的发展现状进行详细探讨。给出近似优化策略的定义、求解流程、特点以及关键技术。对计算试验设计方法、代理模型方法、精度校验与代理模型选择方法等技术进行综述。围绕静态与自适应两类近似优化策略,重点讨论典型的代理模型管理与更新策略与收敛准则。针对飞行器多学科设计优化问题,探讨近似优化策略与分解策略在求解效率与收敛性方面的技术特点。通过数值算例对各项关键技术的特点进行较详尽的对比分析与总结,并依托飞行器设计优化工程实例对近似优化策略的综合性能进行探讨,指出不同近似优化策略的适用范围。研究结果表明,飞行器近似优化策略在优化效率、全局收敛性以及鲁棒性等方面体现出较显著的优势,具有良好的工程应用前景。指出飞行器近似优化策略的未来研究方向。
龙腾刘建WANG G Gary刘莉史人赫郭晓松
关键词:飞行器设计代理模型全局优化
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