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61.
基于共面靶标双目立体视觉传感器标定 总被引:1,自引:0,他引:1
根据双目立体视觉传感器的特点,提出了一种基于共面靶标的双目立体视觉传感器的标定方法.在不需要外部测量设备的情况下,通过共面靶标在平面上自由移动,获得靶标的标定点图像坐标,利用类似于Dr.Janne Heikkil(a)和Dr.Olli Silven所提出来的摄像机内部参数标定模型,采用线性和非线性结合的方法对双目摄像机进行摄像机内部参数的标定.试验结果表明,标定参数与出厂参数有一定的差异,但和实际情况还是吻合的,并且标定方法操作简便,切实可行. 相似文献
62.
本课题的研究内容分为两部分.一部分是对硅压阻式的压力传感测试技术的研究,主要研究的是对硅压阻式压力传感器的主要误差--温度漂移误差和非线性误差进行数字补偿,这是高度速度传感测试技术的基础;另一部分是对低高度小速度传感测试技术的研究,主要研究的是在低高度小速度情况下管路的连接,从而自行研制出高性能的低高度小速度传感器服务于试飞机载测试,来代替进口的高度速度传感器. 相似文献
63.
Abstract. The simultaneous switching autoregressive (SSAR) model proposed by Kunitomo and Sato (A non-linearity in economic time series and disequilibrium econometric models. In Theory and Application of Mathematical Statistics (ed. A. Takemura). Tokyo:University of Tokyo Press (in Japanese), 1994; Asymmetry in economic time series and simultaneous switching autoregressive model. Struct. Change Econ. Dyn. , forthcoming (1994).) is a Markovian non-linear time series model. We investigate the finite sample as well as the asymptotic properties of the least squares estimator and the maximum likelihood (ML) estimator. Due to a specific simultaneity involved in the SSAR model, the least squares estimator is badly biased. However, the ML estimator under the assumption of Gaussian disturbances gives reasonable estimates. 相似文献
64.
Xin Wang 《International journal of systems science》2014,45(7):1393-1401
Missing sensor data is a common problem, which severely influences the overall performance of modern data-intensive control and computing applications. In order to address this important issue, a novel resilient extended Kalman filter is proposed for discrete-time nonlinear stochastic systems with sensor failures and random observer gain perturbations. The failure mechanisms of multiple sensors are assumed to be independent of each other with different failure rates. The locally unbiased robust minimum mean square filter is designed for state estimation under these conditions. The performance of the proposed estimation method is verified by means of numerical Monte Carlo simulation of two different nonlinear stochastic systems, involving a sinusoidal system and a Lorenz oscillator system. 相似文献
65.
In this paper, we aim to solve the finite-horizon optimal control problem for a class of non-linear discrete-time switched systems using adaptive dynamic programming(ADP) algorithm. A new ε-optimal control scheme based on the iterative ADP algorithm is presented which makes the value function converge iteratively to the greatest lower bound of all value function indices within an error according to ε within finite time. Two neural networks are used as parametric structures to implement the iterative ADP algorithm with ε-error bound, which aim at approximating the value function and the control policy, respectively. And then, the optimal control policy is obtained. Finally, a simulation example is included to illustrate the applicability of the proposed method. 相似文献
66.
67.
复杂环境下的多普勒频移变化及信号功率衰减均会对载波准确跟踪造成影响. 在研究北斗卫星B1 频点信号结构的基础上, 建立以环路中相关积分值为观测量的非线性EKF 模型和UKF模型, 并提出利用滤波估计状态量进行状态反馈控制的方法, 从而解决了载波跟踪环路在高动态及弱信号环境中难以高性能工作的问题. 实验结果表明,状态反馈控制的EKF 模型和UKF滤波模型能准确地跟踪弱信号及高动态下的信号变化, 从而有效控制跟踪误差, 为实现快速准确的载波跟踪奠定了基础.
相似文献68.
69.
Student academic underachievement is a concern of paramount importance in Europe, where around 15% of the students in the last high school courses do not achieve the minimum knowledge academic requirement. In this paper, we propose a model based on a system of differential equations to study the dynamics of the students’ academic performance in the German region of the North Rhine-Westphalia. This approach is supported by the idea that both good and bad study habits, are a mixture of personal decisions and influence of classmates. This model allows us to forecast the student academic performance by means of confidence intervals over the next few years. 相似文献
70.
This work shows how to use a differential geometry tool to design a novel nonlinear active fault tolerant flight control system for aircraft. The proposed control scheme consists of two main subsystems: a controller, which is designed for the nominal plant, and a fault detection and diagnosis module, which provides fault estimation. A further feedback loop exploits the fault estimation to accommodate faults affecting the system. The estimate convergence and the stability of the active fault tolerant flight controller are theoretically proved. Finally, high fidelity simulations show the effectiveness of the scheme. 相似文献