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1.
The adaptive optimization of detection thresholds for tracking in clutter is investigated for the probabilistic data association (PDA) filter. Earlier work on this problem by T.E. Fortmann et al. (1985) involved an approximate steady-state analysis of the state error covariance and is only suitable for time-invariant systems. Furthermore, the method requires numerous assumptions and approximations about the error covariance update equation, and uses a cumbersome graphical optimization algorithm. In this work we propose two adaptive schemes for threshold optimization, namely prior and posterior optimization algorithms which minimize the mean-square state estimation error over detection thresholds which depend on data up to the previous and current time-step, respectively. These algorithm are suitable for real-time implementation in time-varying systems. Some simulation results are presented  相似文献   

2.
高斯混合概率假设密度(GM-PHD)滤波是一种基于随机有限集理论的次优贝叶斯多目标跟踪方法,本文研究了该算法在扫描型光学传感器像平面的多目标跟踪问题.针对典型的锥扫模式和推扫模式,根据其扫描特性建立目标的运动模型和测量模型.介绍高斯混合概率假设密度滤波的基本原理.针对原算法在强杂波环境中的低效率问题,借鉴传统多目标跟踪...  相似文献   

3.
A theoretical model of diffuse multipath reflections from rough surfaces is applied to the prediction of multipath power distribu tions in radar coordinates: elevation angle, time delay, and Dop pler frequency. These distributions are used to predict radar tracking errors in elevation angle, for both monopulse and scan ning antenna systems, and typical results are presented. These show a small increase in tracking error for scanning systems, on radially approaching targets, caused by sensitivity of these trackers to amplitude scintillation of the composite direct-plus multipath signal. Effects of knife-edge diffraction and of vegetation ion are briefly considered.  相似文献   

4.
基于输出反馈的柔性航天器变结构跟踪控制方法   总被引:2,自引:2,他引:0  
孙兆伟  叶东  杨正贤  刘源 《航空学报》2010,31(5):1060-1065
为解决柔性航天器姿态机动的控制问题,给出了基于输出反馈的变结构跟踪控制算法。针对柔性航天器的大角度机动,在建立了柔性航天器相对参考轨迹的动力学方程的基础上,设计了仅利用航天器本体的角度和角速度信息的变结构跟踪控制器,使得姿态状态跟踪误差(包括姿态跟踪误差和姿态角速度跟踪误差)以及挠性附件的模态变量从任意的初始状态出发都会到达包含原点的一个闭集内,并且姿态状态跟踪误差能收敛到零,并给出了严格的数学证明。仿真结果证明了所提控制方法的可行性和有效性。  相似文献   

5.
The extended Kalman filter (EKF) has been widely used as a nonlinear filtering method for radar tracking problems. However, it has been found that if cross-range measurement errors of the target position are large, the performance of the conventional EKF degrades considerably due to nonnegligible nonlinear effects. A new filtering algorithm for improving the tracking performance with radar measurements is developed based on the fact that correct evaluation of the measurement error covariance is possible in the Cartesian coordinate system. The proposed algorithm may be viewed as a modification of the EKF in which the variance of the range measurement errors is evaluated in an adaptive manner. The filter structure facilitates the incorporation of the sequential measurement processing scheme, and this makes the resulting algorithm favorable to both estimation accuracy and computational efficiency. Computer simulation results show that the proposed method offers superior performance in comparison to previous methods. Moreover, our developed algorithm provides some useful insight into the radar tracking problem  相似文献   

6.
孙仲康 《航空学报》1984,5(2):118-131
 本文概述了匹配定位原理、方法及相似度度量、快速搜索、正确匹配概率、预处理、几何失真及其改善等问题,还指出了特征匹配及匹配寻的跟踪等两个值得重视的发展趋势。最后给出了相关匹配技术在组合导航及导引头中应用的结构组成。  相似文献   

7.
The authors describe an experimental study of adaptive pointing and tracking control for flexible spacecraft conducted on a complex ground experiment facility. The algorithm used is based on a multivariable direct model reference adaptive control law. Several experimental validation studies performed using this algorithm for vibration damping and robust regulation are extended by addressing the pointing and tracking problem. As is consistent with an adaptive control framework, the plant is assumed to be poorly known to the extent that only system level knowledge of its dynamics is available. Explicit bounds on the steady-state pointing error are derived as functions of the adaptive controller design parameters. It is shown that good tracking performance can be achieved in an experimental setting by adjusting adaptive controller design weightings according to the guidelines indicated by the analytical expressions for the error  相似文献   

8.
Mobile robots are often subject to multiplicative noise in the target tracking tasks, where the multiplicative measurement noise is correlated with additive measurement noise. In this paper,first, a correlation multiplicative measurement noise model is established. It is able to more accurately represent the measurement error caused by the distance sensor dependence state. Then, the estimated performance mismatch problem of Cubature Kalman Filter(CKF) under multiplicative noise is analyzed. An i...  相似文献   

9.
纯方位二维目标跟踪的航迹起始算法   总被引:4,自引:0,他引:4  
陈辉  李晨  连峰 《航空学报》2009,30(4):692-697
 针对传统航迹起始算法在纯方位目标定位和跟踪系统应用中存在的弊端,提出了一种完全基于角度量测的快速航迹起始算法。该方法通过深入分析目标在角度坐标下的运动特性,给出了全新的关联门构造方法。该波门技术有效提高了纯方位二维目标真实量测的确认效率,极大限制了虚假航迹随密集杂波的扩张。利用此波门,通过基于逻辑的方法对仅有角度量测的目标航迹进行扩展。该方法有效地解决了角度坐标系下机动目标的航迹起始分辨率下降的问题,为基于单个被动传感器纯方位跟踪系统进行快速、准确的航迹起始提供了新的思路。仿真结果及实际应用表明了此算法的有效性和实用性。  相似文献   

10.
目标跟踪在自动驾驶和智能监控系统等实时视觉应用中发挥着重要作用。在遮挡、相似干扰等情况下,传统的基于相关滤波的跟踪算法容易发生漂移,鲁棒性有待进一步提高。基于此,提出了一种扩展特征描述的检测辅助核相关滤波目标跟踪架构。首先,在传统的核相关滤波目标跟踪算法的基础上,通过目标检测辅助对跟踪结果进行质量判断,实现对遮挡以及目标丢失的判别;然后通过拓展特征模板的构建与匹配,实现抗干扰相似目标判断及目标重定位;最终,以行人跟踪为例进行了试验,分别通过OTB数据及验证试验和移动机器人平台视觉跟踪验证试验,验证了算法的可行性,并对算法的跟踪性能进行了测试。试验结果表明,所提方法能够稳定地跟踪移动目标,对遮挡、相似干扰具有较强的鲁棒性。  相似文献   

11.
非线性系统中多传感器目标跟踪融合算法研究   总被引:5,自引:1,他引:4  
 研究了在非线性系统中 ,基于转换坐标卡尔曼滤波器的多传感器目标跟踪融合算法。通过分析得出 :在非线性系统的多传感器目标跟踪中 ,基于转换坐标卡尔曼滤波器 ( CMKF)的分布融合估计基本可以重构中心融合估计。仿真实验也证明了此结论。由此可见分布的 CMKFA是非线性系统中较优的分布融合算法  相似文献   

12.
The photovoltaic (PV) generator exhibits a nonlinear i-v characteristic and its maximum power (MP) point varies with solar insolation. In this paper, a V2-based MP point tracking (MPPT) scheme is developed using a buck-boost transformation topology. Although several buck-boost transformation topologies are available we have considered here a coupled inductor SEPIC converter for experimentation. To achieve almost ripple-free array current we have used ripple steering phenomena with the help of integrated inductor. This integrated inductor not only reduces the magnetic core requirements but also improves converter performance. Mathematical models are formulated and tracking algorithm is evolved. A combined PV system simulation model is developed in the SIMULINK. For a given solar insolation, the tracking algorithm changes the duty ratio of the converter such that the solar cell array (SCA) voltage equals the voltage corresponding to the MP point. This is done by the tracking algorithm, which mainly computes the power proportional to square of terminal voltage and changes the duty ratio of the converter so that this power is maximum. The proposed algorithm is implemented in real-time with the help of Analog Device ADMC-401 DSP evaluation module. The tracking program is developed to perform experimental investigations using analog-to-digital converter (ADC) interrupt. Using this processor we are able to track the MP within 200 ms. The proposed peak power tracking effectiveness is demonstrated through simulation and experimental results.  相似文献   

13.
Removal of Out-of-Sequence Measurements from Tracks   总被引:1,自引:0,他引:1  
In multisensor tracking systems that operate in a centralized or distributed information processing architecture, measurements from the same target obtained by different sensors can arrive at the processing center out of sequence due to system latencies. In order to avoid either a delay in the output or the need for reordering and reprocessing entire sequences of measurements, such latent measurements have to be processed by the tracking filter as out-of-sequence measurements (OOSM). Recent work developed a "one-step" procedure for incorporating OOSM with multiple-time-step latency into the tracking filter, which, while suboptimal, was shown to yield results very close to those obtained by reordering and reprocessing an entire sequence of measurements. The counterpart of this problem is the need to remove (revocate) measurements that have already been used to update a track state. This can happen in real-world systems when such measurements are reassigned to another track. Similarly to the problem of update with an OOSM, it is desired to carry out the removal of an earlier measurement without recomputing the track estimate (and the data association) using possibly a long sequence of subsequent measurements one at a time. A one-step algorithm is presented for this problem of removing a multistep OOSM.  相似文献   

14.
主要研究导引头随动系统中探测器信号处理延迟的影响及其补偿控制算法。提出了一种自适应Kalman滤波延迟补偿方案,利用Kalman滤波的预测能力得到当前时刻视线角的估计值,进而得到此时的跟踪误差的估计值,取代被延迟的探测器输出进行闭环控制。考虑到导引头探测器的低更新频率、非等间隔量测等工程特点,又对上述滤波算法进行了一系列改进。仿真表明方法可以明显提高导引头在弹体扰动情况下的跟踪精度。  相似文献   

15.
IMM estimator with out-of-sequence measurements   总被引:3,自引:0,他引:3  
In multisensor tracking systems that operate in a centralized information processing architecture, measurements from the same target obtained by different sensors can arrive at the processing center out of sequence. In order to avoid either a delay in the output or the need for reordering and reprocessing an entire sequence of measurements, such measurements have to be processed as out-of-sequence measurements (OOSMs). Recent work developed procedures for incorporating OOSMs into a Kalman filter (KF). Since the state of the art tracker for real (maneuvering) targets is the interacting multiple model (IMM) estimator, the algorithm for incorporating OOSMs into an IMM estimator is presented here. Both data association and estimation are considered. Simulation results are presented for two realistic problems using measurements from two airborne GMTI sensors. It is shown that the proposed algorithm for incorporating OOSMs into an IMM estimator yields practically the same performance as the reordering and in-sequence reprocessing of the measurements. Also, it is shown how the range rate from a GMTI sensor can be used as a linear velocity measurement in the tracking filter.  相似文献   

16.
基于改进SURF和P-KLT算法的特征点实时跟踪方法研究   总被引:1,自引:0,他引:1  
蔡佳  黄攀峰 《航空学报》2013,34(5):1204-1214
 针对视频序列中运动目标的实时跟踪问题,提出一种基于改进SURF算法和金字塔KLT算法相结合的特征点跟踪方法。首先人工标定目标区域,利用改进的SURF算法分块快速提取具有高鲁棒性、独特性的特征点;然后在后续帧中应用金字塔KLT匹配算法对特征点进行稳定跟踪,采用基于统计的方法剔除错误匹配对;最后利用Greedy Snake分割算法提取轮廓确定更加精准的位置信息,更新目标区域。为使算法更具鲁棒性,还设计了离散点筛选、自适应更新策略。利用飞行视频数据库进行了大量的仿真,结果表明:该算法适用于多尺度图像序列中位置、姿态发生快速变化且结构简单的飞行器的稳定跟踪。帧平均时间为31.8 ms,比SIFT+P-KLT跟踪算法减少47.1%;帧几何中心、目标轮廓面积平均误差分别为5.03像素、16.3%,分别比GFTT+P-KLT跟踪算法减少27.2%、56.9%,比SIFT跟踪算法减少38.6%、68.4%。  相似文献   

17.
针对一类非线性系统的学习控制问题,提出了一种开闭环PD型快速迭代学习控制方法。此学习控制方法利用了系统当前的跟踪误差信号和前次迭代控制的跟踪误差信号,以及它们的微分信号,同时采用可调比例系数,根据系统误差的变化及时地调节比例系数,从而使目标的跟踪能力得到提高。通过分析给出了此快速迭代学习算法收敛的条件,直流电动机的仿真应用说明了此学习控制方法对于非线性系统具有较强的有效性和较好的可行性。  相似文献   

18.
Adaptive robust cubature Kalman filtering for satellite attitude estimation   总被引:2,自引:2,他引:0  
This paper is concerned with the adaptive robust cubature Kalman filtering problem for the case that the dynamics model error and the measurement model error exist simultaneously in the satellite attitude estimation system. By using Hubel-based robust filtering methodology to correct the measurement covariance formulation of cubature Kalman filter, the proposed filtering algorithm could effectively suppress the measurement model error. To further enhance this effect and reduce the impact of the dynamics model error, two different adaptively robust filtering algorithms, one with the optimal adaptive factor based on the estimated covariance matrix of the predicted residuals and the other with multiple fading factors based on strong tracking algorithm, are developed and applied for the satellite attitude estimation. The quaternion is employed to represent the global attitude parameter, and three-dimensional generalized Rodrigues parameters are introduced to define the local attitude error. A multiplicative quaternion error is derived from the local attitude error to maintain quaternion normalization constraint in the filter. Simulation results indicate that the proposed novel algorithm could exhibit higher accuracy and faster convergence compared with the multiplicative extended Kalman filter, the unscented quaternion estimator, and the adaptive robust unscented Kalman filter.  相似文献   

19.
应用卡尔曼滤波的机载雷达跟踪系统   总被引:1,自引:0,他引:1  
毛士艺 《航空学报》1983,4(1):62-72
本文论述将滤波理论应用于机载雷达中对单个目标进行距离、速度、方位角和高低角跟踪的多环反馈系统。首先根据目标和天线的相对运动建立控制四坐标跟踪环所需的状态矢量微分方程,然后推导相应的非线性滤波算法。最后给出计算机的模拟结果。计算机模拟的结果清晰地说明采用最佳滤波的系统性能比通常的有很大改善,并且这种瞄准轴坐标系的最佳系统对目标的随机机动是不灵敏的。 本文所讨论的方法和得出的结论可以延用到地面雷达、舰载雷达以及其他有源和无源的跟踪系统。  相似文献   

20.
We address an optimization problem to obtain the combined sequence of waveform parameters (pulse amplitudes and lengths, and FM sweep rates) and detection thresholds for optimal range and range-rate tracking in clutter. The optimal combined sequence minimizes a tracking performance index under a set of parameter constraints. The performance index includes the probability of track loss and a function of estimation error covariances. The track loss probability and the error covariances are predicted using a hybrid conditional average algorithm. The effect of the false alarms and clutter interference is taken into account in the prediction. A measurement model in explicit form is also presented which is developed based on the resolution cell in the delay-Doppler plane for a single Gaussian pulse. Numerical experiments were performed to solve the optimization problem for several examples.  相似文献   

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