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2014 International Conference on Mechatronics and Control (ICMC)最新文献

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Friction coefficient identification of dry clutch in automated manual transmissions 自动手动变速器干式离合器摩擦系数辨识
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231726
Hongqing Chu, N. Tang, B. Gao, Hong Chen
The friction coefficient identification of dry clutch is a precondition for precise model-based dry clutch control. Recursive Least Square with forgetting factors is adopted to identify the friction coefficient of dry clutch during vehicle starting-up process. Because the accuracy of the engine damp coefficient affects friction coefficient identification of the clutch, it is necessary to identify the clutch friction coefficient and engine damp coefficient simultaneously. Through model simulation, it is shown that accurate and fast identification can be achieved no matter what initial values were chosen. It is also verified that the identification performance is good enough for different launch maneuvers with different throttle operations.
干式离合器摩擦系数的辨识是实现基于模型的干式离合器精确控制的前提。采用带遗忘因子的递推最小二乘法辨识干式离合器起动过程中的摩擦系数。由于发动机阻尼系数的准确性影响离合器摩擦系数的识别,因此有必要同时识别离合器摩擦系数和发动机阻尼系数。通过模型仿真表明,无论选择何种初始值,都能实现准确、快速的识别。验证了在不同的发射机动和不同的油门操作下,该系统的识别性能足够好。
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引用次数: 7
An adaptive-weight regularization method for multi-classifier fusion decision 一种多分类器融合决策的自适应权正则化方法
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231575
Zhu Xufeng, Ma Biao, Guo Guanjun
The difficulties of aircraft type recognition methods are introduced and the necessity of multi-classifier fusion decision method is discussed. The some kinds of invariants: Hu moments, Affine moments, Zernike moments, Wavelet moments, are used for constructing four SVM classifiers. Based on the above four classifiers, an adaptive-weight regularization method is proposed for improving aircraft type classification performance. Experiments are shown that, the recognition rate by the proposed method in this paper is better than any classifier of the above four classifiers, the fixed-weight multi-classifier fusion method and the majority multi-classifier fusion method.
介绍了飞机类型识别方法的难点,讨论了多分类器融合决策方法的必要性。利用Hu矩、仿射矩、Zernike矩、小波矩等不变量构造4个SVM分类器。在以上四种分类器的基础上,提出了一种自适应权值正则化方法来提高飞机型号分类性能。实验表明,本文方法的识别率优于上述四种分类器、固定权值多分类器融合方法和多数多分类器融合方法。
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引用次数: 1
Sampled-data representation for relative motion along elliptical orbits 椭圆轨道相对运动的采样数据表示
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231583
Yafei Li, Genting Yan, Yuzhi Xiao
This paper concerns with the dynamics of TH equations both in the time domain and in the true anomaly domain. Based on the homogeneous solutions of TH equations, a state transition matrix for the TH equations in the true anomaly domain is obtained. The state transition matrix applies to any eccentric orbit. Through the state transition matrix, the sampleddata descriptions are obtained for both the TH equations and the dimensionless equations. In order to evaluate the sampleddata description presented in this paper, a discrete time model constructed by the state transition matrix derived by Melton is introduced. At last simulations present the errors between these sampled-data descriptions.
本文讨论了TH方程在时域和真异常域中的动力学问题。基于TH方程的齐次解,得到了TH方程在真异常域中的状态转移矩阵。状态转移矩阵适用于任何偏心轨道。通过状态转移矩阵,得到了TH方程和无因次方程的采样数据描述。为了评估本文给出的采样数据描述,引入了由Melton导出的状态转移矩阵构造的离散时间模型。最后通过仿真验证了这些采样数据描述之间的误差。
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引用次数: 0
Truss sizing and shape optimization with stress and local buckling constraints 基于应力和局部屈曲约束的桁架尺寸和形状优化
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231851
A. Xiao, Hui Li, Benli Wang
A typical constrained mixed-integer nonlinear program: truss sizing and shape optimization under multi-loading cases and complex constraints is investigated in this work. A laconic adaptive penalty function is employed to handle the structural stress and local buckling constraints. The Covariance Matrix Adaptation Evolution Strategy (CMA-ES) is adopted to update the structural design variables. The effectiveness and efficiency of proposed hybrid algorithm is verified by a benchmark tower optimization problem. Numerical results indicate that the performance indicators of present work are better than those shown in the literature.
研究了一种典型的约束混合整数非线性规划:多载荷和复杂约束条件下桁架的尺寸和形状优化问题。采用简洁的自适应惩罚函数来处理结构应力和局部屈曲约束。采用协方差矩阵自适应进化策略(CMA-ES)更新结构设计变量。通过一个标杆塔优化问题验证了所提混合算法的有效性和高效性。数值结果表明,本文的性能指标优于文献所示。
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引用次数: 0
Relationship between Schur-decomposition based frequency weighted balanced truncation techniques 基于schur分解的频率加权平衡截断技术之间的关系
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231759
V. Sreeram, Xin Du, Xianwei Li
In this paper, we present some remarks on frequency weighted balanced truncation technique based on Schur-decomposition idea. In particular we show that two frequency weighted balanced truncation techniques [7], [9] based on Schur-decomposition idea are special cases of a more general technique introduced recently in [10], [11].
本文对基于舒尔分解思想的频率加权平衡截断技术作了一些评述。我们特别指出,基于schur分解思想的两种频率加权平衡截断技术[7],[9]是最近在[10],[11]中引入的一种更一般的技术的特殊情况。
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引用次数: 0
Classification of optical music symbols based on combined neural network 基于组合神经网络的光学音乐符号分类
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231590
Cuihong Wen, Ana Rebelo, J. Zhang, Jaime S. Cardoso
In this paper, a new method for music symbol classification named Combined Neural Network (CNN) is proposed. Tests are conducted on more than 9000 music symbols from both real and scanned music sheets, which show that the proposed technique offers superior classification capability. At the same time, the performance of the new network is compared with the single Neural Network (NN) classifier using the same music scores. The average classification accuracy increased more than ten percent, reaching 98.82%.
本文提出了一种新的音乐符号分类方法——组合神经网络(CNN)。对真实乐谱和扫描乐谱中的9000多个音乐符号进行了测试,结果表明该方法具有较好的分类能力。同时,将新网络的性能与使用相同乐谱的单个神经网络(NN)分类器进行了比较。平均分类准确率提高了10%以上,达到98.82%。
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引用次数: 7
Beam pattern analysis based on sensor distribution in uncertain environment 不确定环境下基于传感器分布的波束方向图分析
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231876
Jian Hou, Long Xiao, Lei Li, Zhun Liu, Xiaoqin Ji, Lei Gao
This paper addresses the beam pattern analysis in uncertain environment. Assuming that beamforming is achieved along one given receiver direction, the beam pattern is controlled via the sensor distribution to make different goals. Given two different applications, we show that the sensor nodes are located in a straight line perpendicular to the receiver direction, different distance between the sensors contributes towards separate purposes, respectively. Simulation results are provided to validate the effectiveness of our approach.
本文研究了不确定环境下的光束方向图分析。假设波束形成沿一个给定的接收器方向,波束方向通过传感器分布来控制以达到不同的目标。给定两种不同的应用,我们表明传感器节点位于垂直于接收器方向的直线上,传感器之间的不同距离分别有助于不同的目的。仿真结果验证了该方法的有效性。
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引用次数: 0
Design and simulation of highway traffic information collection based on wireless network 基于无线网络的公路交通信息采集系统设计与仿真
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231828
Chuanxiang Ren, Fasheng Liu, Xiao Lu, Hongqiang Sun
With the wireless network and mobile Internet development, the mobile phones are rapidly developed and more popular, and so it's becoming possible to get highway traffic information by locating the mobile phones in vehicles. The system structure for the highway traffic information collection is designed based on wireless network and mobile phones in vehicles, and the vehicle recognition and its information computation methods are given and discussed. Also the simulation is done for vehicle recognition and computation based on fuzzy cluster analysis method and the results are got and analyzed.
随着无线网络和移动互联网的发展,移动电话得到了迅速的发展和普及,因此通过手机在车辆中的定位来获取公路交通信息已经成为可能。设计了基于无线网络和车载手机的公路交通信息采集系统结构,给出并讨论了车辆识别及其信息计算方法。对基于模糊聚类分析方法的车辆识别和计算进行了仿真,并对仿真结果进行了分析。
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引用次数: 0
The design of AOCS software architecture in micro-satellite using software bus 基于软件总线的微卫星AOCS软件体系结构设计
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231814
Chen Jian, N. Ming-feng, Yang Run-dong, Sun Zhao-wei, Xu Guo-dong
A new attitude and orbit control system (AOCS) software architecture is presented in this paper by using the concept of software bus. According to the analysis of the function flow and data flow of AOCS, its software components are partitioned clearly under the rule of function cohesion and data cohesion, and each component data interaction standard interface is determined as well. Based on such kind of partition, a series of software components with single function are developed to build a component library, which is used for function configuration of AOCS software. Finally, using this library, desired AOCS software can be integrated to follow the mission requirement. During the integration, the software bus is chosen as the communication style of the software architecture to dispatch and manage the components of the software.
利用软件总线的概念,提出了一种新的姿态与轨道控制系统软件体系结构。通过对AOCS的功能流和数据流的分析,按照功能内聚和数据内聚的原则对其软件组件进行了清晰的划分,并确定了各组件数据交互的标准接口。在这种划分的基础上,开发了一系列功能单一的软件组件,构建了一个组件库,用于AOCS软件的功能配置。最后,利用该库可以集成所需的AOCS软件,以满足任务需求。在集成过程中,选择软件总线作为软件体系结构的通信方式,对软件组件进行调度和管理。
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引用次数: 0
SINS/CNS/GNSS integrated navigation scheme for advanced upper stage 高级上级SINS/CNS/GNSS组合导航方案
Pub Date : 2014-07-03 DOI: 10.1109/ICMC.2014.7231938
Hua Zong, Zhun Liu, Xiaoying Gao, Bo Wang, Sen Wang, Da Xu
A SINS/CNS/GNSS integrated navigation scheme is researched for advanced upper stage in this paper. First of all, the composition of the integrated navigation is introduced. Then, the error model of the integration system in launch inertial frame was established. especially the misalignments of star tracker are inputted as system states, and also the federated filter algorithm is used to estimate the state errors of the integrated navigation system. Finally, simulations results show that the SINS/CNS/GNSS integrated navigation can provide navigation parameters with high accuracy, which can meet the accuracy requirements of advanced upper stage.
本文研究了一种SINS/CNS/GNSS组合导航方案。首先,介绍了组合导航系统的组成。在此基础上,建立了集成系统在发射惯性坐标系下的误差模型。特别是将星跟踪器的失调作为系统状态输入,并采用联邦滤波算法对组合导航系统的状态误差进行估计。最后,仿真结果表明,SINS/CNS/GNSS组合导航能够提供高精度的导航参数,满足高级上级的精度要求。
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引用次数: 1
期刊
2014 International Conference on Mechatronics and Control (ICMC)
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