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激光陀螺捷联惯性导航系统中惯性器件误差补偿技术 被引量:28
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作者 熊智 刘建业 +1 位作者 林雪原 曾庆化 《上海交通大学学报》 EI CAS CSCD 北大核心 2003年第11期1795-1799,共5页
为了提高激光捷联惯性导航系统的导航精度,对惯性器件误差进行了原理上的分析和说明,并针对由国内某型激光陀螺构成的惯性测量器件进行了误差分析.在此基础上建立了误差补偿的精确数学模型,提出了一种简易的且具有较高精度的误差模型参... 为了提高激光捷联惯性导航系统的导航精度,对惯性器件误差进行了原理上的分析和说明,并针对由国内某型激光陀螺构成的惯性测量器件进行了误差分析.在此基础上建立了误差补偿的精确数学模型,提出了一种简易的且具有较高精度的误差模型参数静态标定方法,给出了计算误差模型参数的数学推导过程和解析表达式.分析结果表明,惯导系统误差主要由惯性器件测量误差引起,为了有效补偿惯导系统的系统误差,必须针对具体的惯性器件进行误差补偿.实际测试结果证明,该计算方法精度较高,可以有效提高惯导精度. 展开更多
关键词 误差补偿 静态标定 激光陀螺 捷联惯性
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基于递归神经网络模型的传感器非线性动态补偿 被引量:9
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作者 田社平 《上海交通大学学报》 EI CAS CSCD 北大核心 2003年第1期13-16,共4页
讨论了递归神经网络模型在传感器非线性动态补偿中的应用 ,给出了递归神经网络模型的结构及相应的训练算法 .递归神经网络模型本身具有动态映射能力 ,其结构仅与输入层和中间层的节点数有关 ,且不需要知道被补偿传感器的结构特性 (如输... 讨论了递归神经网络模型在传感器非线性动态补偿中的应用 ,给出了递归神经网络模型的结构及相应的训练算法 .递归神经网络模型本身具有动态映射能力 ,其结构仅与输入层和中间层的节点数有关 ,且不需要知道被补偿传感器的结构特性 (如输出、输入的最大延迟 )等先验知识 ,简化了动态补偿器的结构设计 .采用递推预报误差算法训练神经网络 ,具有收敛速度快、收敛精度高的特点 .实验结果表明 ,经过补偿后的传感器具有期望的输入输出特性 。 展开更多
关键词 传感器 非线性动态补偿 递归神经网络模型 网络结构 训练算法 递推预报误差算法
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Observer-based backstepping longitudinal control for carrier-based UAV with actuator faults 被引量:9
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作者 Fengying Zheng Ziyang Zhen Huajun Gong 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2017年第2期322-337,共16页
The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output... The paper presents the longitudinal control for the carrier-based unmanned aerial vehicle (UAV) system with unmeasured states, actuator faults, control input constraints, and external disturbances. By combining output state observer, adaptive fuzzy control, and constraint backstepping technology, a robust fault tolerant control approach is proposed. An output state observer with fuzzy logic systems is developed to estimate unmeasured states, and command filters rather than differentiations of virtual control law are used to solve the computational complexity problem in traditional backstepping. Additionally, a robust term is introduced to offset the fuzzy adaptive estimation error and external disturbance, and an appropriate fault controller structure with matching conditions obtained from fault compensation is proposed. Based on the Lyapunov theory, the designed control program is illustrated to guarantee that all the closed-loop signals of the given system are bounded, and the output errors converge to a small neighborhood of zero. A carrier-based UAV nonlinear longitudinal model is employed to testify the feasibility and validity of the control scheme. The simulation results show that all the controllers can perform at a satisfactory level of reference tracking despite the existence of unknown aerodynamic parameters and actuator faults. © 2017 Beijing Institute of Aerospace Information. 展开更多
关键词 Actuators Aircraft control BACKSTEPPING Control system analysis Control theory Controllers error compensation Fault tolerance Flight control systems Fuzzy control Fuzzy filters Fuzzy logic State estimation Three term control systems Unmanned aerial vehicles (UAV)
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高精度测试转台鉴相型测角系统动态误差的自动补偿 被引量:4
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作者 王茂 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 2001年第5期628-631,共4页
在惯导测试转台中 ,测角系统是影响其精度的一个最主要因素 .而目前常用的鉴相测角系统只能保证其静态精度 .当测角线路中存在参数动态变化以及转台运动时 ,测角系统精度将有很大损失 ,因而难以保证测试转台有较高的动态精度 .为此详细... 在惯导测试转台中 ,测角系统是影响其精度的一个最主要因素 .而目前常用的鉴相测角系统只能保证其静态精度 .当测角线路中存在参数动态变化以及转台运动时 ,测角系统精度将有很大损失 ,因而难以保证测试转台有较高的动态精度 .为此详细分析了双相激磁鉴相型测角系统的动态误差来源及表现形式 ,提出了一种闭环自动补偿方案 ,并给出了其具体实现电路 ;经过分析和实验 ,证明该方案不仅通用效抑制测角线路参数变化的影响 ,而且可以保证转台运动中相位自动完全补偿 ,从而不仅能进一步提高测角系统静态精度 ,而肫可使其动态精度达到 1″以内 . 展开更多
关键词 惯导测试转台 测角系统 误差补偿 动态误差 静态精度 动态精度 感应同步器
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视觉引导抓取机械手工作平面定位误差与修正 被引量:2
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作者 王向军 陈思伟 《机械科学与技术》 CSCD 北大核心 2015年第5期720-723,共4页
采取视觉的方法对工作台上的产品定位,提出了1种空间已知平面上的点的定位误差模型。首先,建立单目视觉定位模型,得出工作台平面上的点的横纵坐标与该点的像面坐标之间的关系,实现该平面上的点定位。然后,根据径向畸变模型建立定位误差... 采取视觉的方法对工作台上的产品定位,提出了1种空间已知平面上的点的定位误差模型。首先,建立单目视觉定位模型,得出工作台平面上的点的横纵坐标与该点的像面坐标之间的关系,实现该平面上的点定位。然后,根据径向畸变模型建立定位误差模型。最后,通过实验,对工作台平面上144个角点进行定位,用这144个角点的定位误差数据拟合该定位误差模型中的待定系数,并用最终确立的定位误差模型补偿144个角点定位误差。实验结果显示:该定位误差模型的两个待定常数的拟合确定系数高达0.9以上,经过定位误差模型补偿修正以后,工作台平面144个角点的两个坐标方向的最大定位误差由2.15 mm、1.94 mm显著降低到0.62 mm、0.29 mm。实验结果证明提出的单目视觉定位误差模型的正确性,并证明了影响成像系统畸变的主要因素是径向畸变。 展开更多
关键词 单目视觉 定位误差 径向畸变 拟合
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Coarse error analysis and correction of a two-dimensional triangulation range finder 被引量:1
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作者 桂华侨 吕亮 +6 位作者 黄伟 徐军 何德勇 王焕钦 谢建平 赵天鹏 明海 《Chinese Optics Letters》 SCIE EI CAS CSCD 2006年第2期84-86,共3页
A real-time two-dimensional (2D) triangulation range finder is presented, which is composed of two linear complementary metal oxidation semiconductor (CMOS) chips, two camera lenses, and four light emitting diodes... A real-time two-dimensional (2D) triangulation range finder is presented, which is composed of two linear complementary metal oxidation semiconductor (CMOS) chips, two camera lenses, and four light emitting diodes (LEDs). The high order distortion in image aberrations is the main factor responsible for the coarse errors. The theoretical prediction is in good agreement with experiments and the correction equation is used to obtain more reliable results with the unique distortion coefficient in tile whole working region. 展开更多
关键词 Camera lenses Distortion (waves) error analysis Image processing Light emitting diodes Microprocessor chips MOS devices Optical instruments Real time systems TRIANGULATION Two dimensional
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STUDY ON GAIN-SCHEDULING PROBLEM IN FLIGHT CONTROL 被引量:1
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作者 高建平 陈宗基 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1999年第4期217-221,共5页
Gain-scheduling has got its wide applications in modern flight control, in which control gains are scheduled with variables such as dynamic pressure and Mach number, to meet dynamic response requirements in different ... Gain-scheduling has got its wide applications in modern flight control, in which control gains are scheduled with variables such as dynamic pressure and Mach number, to meet dynamic response requirements in different flight conditions. Classical gain-scheduling approaches may result in some problems, which can not guarantee global robustness and stability in transitions of different flight conditions. Gain-scheduling problem is systematically investigated from robustness point of view in the paper. Detailed procedures for gain-scheduled controller to achieve both robustness and stability performance are given and applied to a typical flight control system. For switching stability problems of different flight conditions in flight control systems, a new approach is proposed, in which different flight conditions are reduced into a parameter varying plant using interpolation firstly, and then parameter-varying controller design goes next. Though interpolation errors may exist, the robust parameter varying controller design can compensate for those uncertainties and errors, and finally achieve good performance of robustness and switching stability during transitions. Illustrative simulation at last shows satisfactory results. 展开更多
关键词 error analysis Gain control INTERPOLATION Parameter estimation PROBABILITY Robustness (control systems) System stability
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Computation Method for the Real-Time Control Problems in Differential-Algebraic Systems
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作者 Fei, Jinggao 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 1999年第2期20-28,共9页
In this paper, a real-time computation method for the control problems in differential-algebraic systems is presented. The errors of the method are estimated, and the relation between the sampling stepsize and the con... In this paper, a real-time computation method for the control problems in differential-algebraic systems is presented. The errors of the method are estimated, and the relation between the sampling stepsize and the controlled errors is analyzed. The stability analysis is done for a model problem, and the stability region is ploted which gives the range of the sampling stepsizes with which the stability of control process is guaranteed. 展开更多
关键词 ALGEBRA Computational complexity Computer control systems error analysis Mathematical models Process engineering Production engineering Real time systems Sampling System stability
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Study of a New Method of Tracking Control with Zero Steady-State Error on Very-Low Frequency
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作者 肖卫国 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2001年第4期66-70,共5页
A servo control system is prone to low speed and unsteadiness during very-low-frequency follow-up. A design method of feedforward control based on intelligent controller is put foward. Simulation and test results show... A servo control system is prone to low speed and unsteadiness during very-low-frequency follow-up. A design method of feedforward control based on intelligent controller is put foward. Simulation and test results show that the method has excellent control characteristics and strong robustness, which meets the servo control needs with very-low frequency. 展开更多
关键词 Computer simulation error analysis Intelligent control Robustness (control systems)
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NONLINEAR FILTERING ALGORITHM FOR IN S INITIAL ALIGNMENT
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作者 王丹力 张洪钺 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 1999年第4期246-250,共5页
The initial alignment error equation of an INS (Inertial Navigation System) with large initial azimuth error has been derived and nonlinear characteristics are included. When azimuth error is fairly small, the nonline... The initial alignment error equation of an INS (Inertial Navigation System) with large initial azimuth error has been derived and nonlinear characteristics are included. When azimuth error is fairly small, the nonlinear equation can be reduced to a linear one. Extended Kalman filter, iterated filter and second order filter formulas are derived for the nonlinear state equation with linear measurement equation. Simulations results show that the accuracy of azimuth error estimation using extended Kalman filter is better than that of using standard Kalman filter while the iterated filter and second order filter can give even better estimation accuracy. 展开更多
关键词 Algorithms error analysis Inertial navigation systems Iterative methods Nonlinear equations Nonlinear filtering Parameter estimation
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基于误差状态量的卡尔曼滤波器在SINS+GPS组合导航中的应用 被引量:1
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作者 羊彦 侯小林 +1 位作者 张杨 景占荣 《西北工业大学学报》 EI CAS CSCD 北大核心 2011年第5期685-689,共5页
卡尔曼滤波(KF)在SINS+GPS组合制导方法中应用广泛,但是运载体的传感器数学模型一般为非线性,其模型复杂度和运算量较大。文章提出了SINS+GPS组合制导中基于误差状态量的卡尔曼滤波算法,为了回避非线性所带来的复杂性,将GPS数据与惯性... 卡尔曼滤波(KF)在SINS+GPS组合制导方法中应用广泛,但是运载体的传感器数学模型一般为非线性,其模型复杂度和运算量较大。文章提出了SINS+GPS组合制导中基于误差状态量的卡尔曼滤波算法,为了回避非线性所带来的复杂性,将GPS数据与惯性导航数据的误差作为状态量,由于误差的数学模型为线性,明显降低了设计难度。文中给出了设计过程和导航系统的数学模型,对该模型的状态参数进行了设置,最后用仿真试验证明了该算法的有效性。 展开更多
关键词 算法 分析 设计 误差模型 反馈 全球定位系统(GPS) 惯性导航系统 卡尔曼滤波(KF) 模型 参数估计 传感器 仿真 捷联式惯性导航系统(SINS)
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错误集
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作者 郭开仲 张式强 《广东工业大学学报》 CAS 1990年第1期1-7,共7页
本文为了研究错误的理论和定量化描述错误的需要,在文[1]的基础上提出了“错误”集的概念,并讨论“错误”集的分类,几种运算及其规律和研究方向。
关键词 错误 错误系统分析 错误集
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阵列误差对MUSIC算法性能的影响与校正 被引量:31
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作者 韩芳明 张守宏 潘复平 《西安电子科技大学学报》 EI CAS CSCD 北大核心 2003年第5期585-589,共5页
理论上分析了阵元增益误差和相位误差对基于子空间分解的MUSIC算法进行DOA估计性能的影响,在此基础上给出了一种基于最大似然估计的Toeplitz化通用自校正方法.该方法利用理想阵列协方差矩阵的Toeplitz性质,无需估计误差而可以对其作出补... 理论上分析了阵元增益误差和相位误差对基于子空间分解的MUSIC算法进行DOA估计性能的影响,在此基础上给出了一种基于最大似然估计的Toeplitz化通用自校正方法.该方法利用理想阵列协方差矩阵的Toeplitz性质,无需估计误差而可以对其作出补偿.仿真结果表明该方法不但可以减少MUSIC方法对阵列误差的敏感性,而且可以进一步降低其信噪比门限. 展开更多
关键词 阵列误差 MUSIC算法 DOA估计 最大似然估计 稳健性
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Local Influence on the Error-Correction Variable in a Cointegrated System
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作者 Zhang, X. Yang, B. +1 位作者 Zhang, T. Zhang, S. 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2001年第3期1-8,共8页
The concept of cointegration describes an equilibrium relationship among a set of time-varying variables, and the cointegrated relationship can be represented through an error-correction model (ECM). The error-correct... The concept of cointegration describes an equilibrium relationship among a set of time-varying variables, and the cointegrated relationship can be represented through an error-correction model (ECM). The error-correction variable, which represents the short-run discrepancy from the equilibrium state in a cointegrated system, plays an important role in the ECM. It is natural to ask how the error-correction mechanism works, or equivalently, how the short-run discrepancy affects the development of the cointegrated system? This paper examines the effect or local influence on the error-correction variable in an error-correction model. Following the argument of the second-order approach to local influence suggested by reference [5], we develop a diagnostic statistic to examine the local influence on the estimation of the parameter associated with the error-correction variable in an ECM. An empirical example is presented to illustrate the application of the proposed diagnostic. We find that the short-run discre pancy may have strong influence on the estimation of the parameter associated with the error-correction model. It is the error-correction variable that the short-run discrepancies can be incorporated through the error-correction mechanism. 展开更多
关键词 Computer simulation error correction Mathematical models Parameter estimation Program diagnostics Statistical methods Time series analysis Time varying control systems
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