共查询到20条相似文献,搜索用时 218 毫秒
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图像分割是合成孔径雷达(Synthetic Aperture Radar, SAR)图像自动解译技术中的一个重要问题。基于活动轮廓的思想,给出了一种适应于SAR图像分割的集成活动轮廓模型。该模型综合利用SAR图像的边缘和区域特性,通过检测算子提取SAR图像的边缘信息,利用似然函数的最大化提取图像中不同统计信息的区域;通过边缘和区域的共同曲线运动实现对SAR图像的分割。利用加性算子分裂算法,给出了该模型的快速实现方法。通过MSTAR和实测星载SAR数据进行试验验证,并与其他算法比较,结果表明:所提方法适应性强,可适应复杂背景的SAR图像分割,并且分割定位准确、收敛速度较快;所提实现算法稳健,能适应不同参数设置,且对初始条件不敏感。〖JP〗 相似文献
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改进模糊马尔可夫随机场的SAR图像分割 总被引:1,自引:0,他引:1
模糊马尔可夫随机场利用模糊隶属度函数解决了马尔可夫随机场过于依赖灰度值的弊 端,然而在模糊马尔可夫随机场的分割中采用的是硬性基团和边缘判断准则,模糊分类使得 这些判断条件更加难以满足,从而图像分割中容易产生边缘分割错误的现象。改进模糊马尔 可夫随机场是在分段模糊马尔可夫随机场中引入模糊意义的后验概率公式及基团和边缘类型 “模糊相似性”概念,通过对不同基团和边缘类型的模糊相似性描述与判断,使得图像分割 对于边缘的判断和噪声的抑制具有更好的效果。仿真实验表明改进模糊马尔可夫随机场对于 边缘特别模糊的合成孔径雷达图像(SAR)具有较好的分割效果。 相似文献
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This paper presents the sample return mission to a primitive Near-Earth Asteroid (NEA) MarcoPolo-R proposed to the European Space Agency in December 2010. MarcoPolo-R was selected in February 2011 with three other missions addressing different science objectives for the two-year Assessment Phase of the Medium-Class mission competition of the Cosmic Vision 2 program for launch in 2022. The baseline target of MarcoPolo-R is the binary NEA (175706) 1996 FG3, which offers an efficient operational and technical mission profile. A binary target also provides enhanced science return. The choice of a binary target allows several scientific investigations to occur more easily than through a single object, in particular regarding the fascinating geology and geophysics of asteroids. MarcoPolo-R will rendezvous with a primitive, organic-rich NEA, scientifically characterize it at multiple scales, and return a bulk sample to Earth for laboratory analyses. The MarcoPolo-R sample will provide a representative sample from the surface of a known asteroid with known geologic context, and will contribute to the inventory of primitive material that is probably missing from the meteorite collection. The MarcoPolo-R samples will thus contribute to the exploration of the origin of planetary materials and initial stages of habitable planet formation, to the identification and characterization of the organics and volatiles in a primitive asteroid and to the understanding of the unique geomorphology, dynamics and evolution of a binary asteroid that belongs to the Potentially Hazardous Asteroid (PHA) population. 相似文献
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为确定失效航天器等非合作目标的相对位姿,提出一种通过纹理边界检测的椭圆特征提取方法。该方法假设椭圆特征是航天器表面两种不同纹理的边界,利用上一时刻相对位姿信息,将对接环离散几何模型投影到像平面,并沿各离散点的法向方向通过概率方法检测纹理边界点。利用随机抽样一致(RANSAC)方法剔除边界点中的粗大误差,进而拟合出椭圆参数。纹理特征对光照变化具有鲁棒性,因此该方法能够在变光照、星体表面反光不均匀等复杂情况下快速准确地提取图像中的椭圆特征。本文以对接环图像特征提取为例进行仿真校验,分析了算法参数和噪声对提取椭圆精度和时间的影响。利用真实图像与基于梯度边缘的椭圆提取方法进行对比,结果表明,所提出的算法具有较高的精度和速度。 相似文献
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Fault detection,identification and reconstruction for gyroscope in satellite based on independent component analysis 总被引:1,自引:0,他引:1
Although satellites are designed with high reliability, faults do occur when satellites are in orbit. To avoid the important services being affected, redundancy is used in satellites. There are many sensors in satellites. In order to reduce the cost, space, weight and power consumption, redundant sensors should be added to satellite as few as possible. Analytical redundancy is an efficient way to optimize the application of redundant. The gyroscope is the attitude determination sensor of the satellite. The minimum redundant structure of the gyroscope system is as follows: three gyroscopes installed in three-axis orthogonally and one gyroscope installed with slantwise for redundancy(3o+1S).To achieve fault detection, identification and reconstruction, hypothesis of statistical independence between the three-axis angular rates and hypothesis of statistical independence between the angular rates and fault are proposed. The scenario that only one sensor is faulting and there are only additive fault and full fault is supposed. Under these assumptions, firstly a threshold method is used for fault detection. After a fault is detected, independent component analysis (ICA) based algorithm for fault identification is employed. To overcome the ambiguities of ICA, correlation coefficients and prior information of the mixed matrix are used. Finally, the reconstruction matrix is obtained. By using this matrix fault signal is extracted so that the yaw, roll and pitch axes (three-axis) angular rates of the satellite can be recovered. Numerical simulations show this method can fulfill fault detection, identification and reconstruction of the gyroscope system. 相似文献
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根据瞬时速度脉冲、逐段常量经验加速度和周期性摄动加速度模型的特点,分别给出敏感矩阵的有效计算方法,以及最小二乘批处理的设计矩阵和法方程矩阵的分块结构。该建模方法将灵敏度矩阵数值积分规模和存储规模降为O(n),而传统方法为O(n 2)。应用GRACE-A星载GPS观测数据对法方程的计算效率测试,结果表明:对于瞬时速度脉冲和逐段常量经验加速度模型,当采用伪距观测量时,法方程构建效率提高1倍;当采用伪距加载波相位观测量时,效率提高3.5倍。对于周期性摄动加速度模型,效率没有明显提高,主要原因在于模型参数较少,矩阵分块建模方法的优越性尚未体现。 相似文献
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针对日地L2平动点相对运动拟线性变参数(QLPV)动力学模型,提出一种改进的多项式特征结构配置(PEA)方法实现日地L2平动点编队飞行高精度相对位置保持.建立日地L2平动点编队飞行相对运动QLPV动力学模型,将基于线性时不变系统(LTI)的PEA方法进行改进,设计参数/状态变化的控制方法来获取闭环系统设计传递函数,与期望传递函数进行类似于线性系统的条件匹配,获得含时变参数和状态的多项式控制器,确保系统在参数和状态变化时能保持控制系统性能不变.在进行多输入多输出(MIMO)系统的算法设计时,将系统期望传递函数设为解耦形式,实现飞行器三轴位置间的解耦控制,以确保系统的控制精度.考虑到拟线性变参数系统与传统线性系统的不同,对拟线性变参数闭环系统的稳定性进行分析.最后进行了相应的数学仿真验证算法的可行性和有效性. 相似文献
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A special measurement technique allows to determine the stationary and dynamic temperature profiles, acting on a material sample during a Bridgman crystal growth process. It turns out that the thermal field of the furnaces at the place of the sample is modified by a number of device-related factors and by regular correlations. The investigations refer to the execution of experiments in the field of materials sciences in space in furnaces on board Salyut-stations. 相似文献
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象移对星载TDICCD相机成像品质的影响分析 总被引:1,自引:0,他引:1
像移是影响星载时间延迟积分电荷耦合器件(TDICCD)相机成像品质的重要因素。为研究像移对TDICCD像质的影响,首先分析了像移引起图像模糊和几何变形的机理,研究了像移降质的辐射和几何方面评价参量。依据TDICCD工作原理,建立了像移影响下TDICCD相机空变降质模型,并以此为基础,计算并分析了不同形式、不同方向上的像移影响下的像质下降情况。分析结果表明,不同方向、不同形式的像移引起的成像品质下降是不同的。文章中提出的空变降质模型可以为后续的仿真及像移降质图像的恢复等提供参考。 相似文献
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S. Yu. Ulybyshev 《Cosmic Research》2016,54(4):303-312
We present a method for designing nonuniform satellite systems for continuous global coverage using a combination of equatorial and near-polar satellite segments in circular orbits. Equations are derived to determine the basic design parameters of the satellite system itself and the conditions of its closure at the joint of near-polar and equatorial segments. We analyze specific features of near-polar and equatorial satellite systems and their advantages and disadvantages compared with existing classes of near-polar phased and kinematically correct satellite systems. We estimate the minimum required number of spacecrafts in satellite systems for a given fold of coverage and present calculated dependences for classes of near-polar phased and equatorial satellite systems with different types of closure. For the class of kinematically correct satellite systems, we analyze the characteristics of systems with a minimum spacecraft flight height and reveal that the number of satellites in the orbital plane depends on the flight height for different folds of coverage. We bring examples of the best near-polar equatorial satellite systems of global coverage for different folds and a class of satellite systems with a fixed number of spacecrafts and orbital planes in them. 相似文献