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Image mosaicking is widely used in Geographic Information Systems (GISs) for large-scale ground surface analysis. However, most existing mosaicking methods can only be used in offline processing due to the enormous amounts of computation. In this paper, we propose a novel and practical algorithm for real-time infrared video mosaicking. To achieve this, a novel fast template matching algorithm based on Sum of Cosine Differences (SCD) is proposed to coarsely match the sequential images. The high speed of the proposed template matching algorithm is obtained by computing correlation with Fast Fourier Transform (FFT). We also propose a novel fast Least Squares Matching (LSM) algorithm for inter-frame fine registration, which can significantly reduce the computation without degrading the matching accuracy. In addition, the proposed fast LSM can effectively adapt for noise degradation and geometric distortion. Based on the proposed fast template matching algorithm and fine registration algorithm, we develop a practical real-time mosaicking approach which can produce seamless mosaic image highly efficiently. Experiments on synthetic and real-world datasets demonstrate that the proposed algorithm is not just computationally efficient but also robust against various noise distortions. 相似文献
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SAR多运动目标的检测和参数估计较单运动目标的难度大大增加,传统的WVD方法在处理多分量线性 调频信号时存在交叉项干扰的问题,改进的WVD-HT方法可减弱交叉项的影响,但并不能从根本上解决交叉项问题, 同时计算量也很大。文中提出一种基于分数阶Fourier域滤波的多运动目标检测和参数估计方法,在运动目标和静止目 标信号分离后通过逐个消去强目标信号,有效地解决了弱目标信号的检测和参数估计问题,由于分数阶Fourier变换是 线性变换,从而免除了交叉项的困扰。仿真和实测数据的处理结果验证了算法的有效性。 相似文献
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某测试台主要运动方式为三自由度正弦摇摆Asinωt,三次谐波摇摆。本文详细阐述了该设备三次谐波谱的精密运动控制、在线实时轨迹显示和静态FFT分析。 相似文献
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针对航天器小推力转移轨迹的初始设计问题,利用基于三阶Fourier级数的设计方法实现了航天器小推力的多圈转移。同时,基于有限Fourier级数的形状法,对具有多个约束条件的小推力多圈转移轨迹进行了优化设计。选取了共面同轴同偏心率的初始和末端轨道位置,对所提出的方法进行了仿真验证。结果表明:与改进逆五阶多项式形状法相比,所提出的方法虽然增加了转移时间,但当转移圈数为5圈、有限Fourier级数的项数为10时,可减少将近75%的转移速度增量,同时大大减小了所需的最大推力加速度的值。 相似文献
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Ehsan Taheri Ilya Kolmanovsky Ella Atkins 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(3):879-890
Shape-based methods are becoming popular in low-thrust trajectory optimization due to their fast computation speeds. In existing shape-based methods constraints are treated at the acceleration level but not at the thrust level. These two constraint types are not equivalent since spacecraft mass decreases over time as fuel is expended. This paper develops a shape-based method based on a Fourier series approximation that is capable of representing trajectories defined in spherical coordinates and that enforces thrust constraints. An objective function can be incorporated to minimize overall mission cost, i.e., achieve minimum . A representative mission from Earth to Mars is studied. The proposed Fourier series technique is demonstrated capable of generating feasible and near-optimal trajectories. These attributes can facilitate future low-thrust mission designs where different trajectory alternatives must be rapidly constructed and evaluated. 相似文献