海洋一号C(HY-1C)卫星是中国首颗海洋水色业务卫星,其搭载的海岸带成像仪(Coastal Zone Imager, CZI)具有大幅宽、短重访周期的优势,可实现海洋和海岸带的大面积观测。作为光学传感器,CZI受云影响严重,准确识别云是CZI数据处理的关键,但...海洋一号C(HY-1C)卫星是中国首颗海洋水色业务卫星,其搭载的海岸带成像仪(Coastal Zone Imager, CZI)具有大幅宽、短重访周期的优势,可实现海洋和海岸带的大面积观测。作为光学传感器,CZI受云影响严重,准确识别云是CZI数据处理的关键,但是CZI缺少红外和短波红外等对云敏感的波段,云检测难度大。针对该问题,本文提出一种融合多尺度卷积和侧窗滤波的轻量化云检测方法,该方法通过多尺度卷积获取云的不同尺度特征,通过侧窗滤波突出边缘特征,减少椒盐噪声的影响,提升云边缘检测的精度。实验结果表明,本文所提出的方法可有效进行云检测,在云边缘提取方面表现较好,F1-score达92.77%,Kappa系数达0.89,与现有云检测方法相比优势明显,且模型训练速度快、参数量少,可为HY-1C CZI遥感影像处理提供有力支撑。展开更多
This paper considers the guidance and control problem of a flight vehicle with sidewindow detection. In order to guarantee the target remaining in the seeker＇s sight of view, the line of sight and the attitude of the...This paper considers the guidance and control problem of a flight vehicle with sidewindow detection. In order to guarantee the target remaining in the seeker＇s sight of view, the line of sight and the attitude of the flight vehicle should be under some constraints caused by the sidewindow, which leads to coupling between the guidance and the attitude dynamics model. To deal with the side-window constraints and the coupling, a novel Integrated Guidance and Control（IGC）design approach is proposed. Firstly, the relative motion equations are derived in the body-Line of Sight（LOS） coordinate system. And the guidance and control problem of the flight vehicle is formulated into an IGC problem with state constraints. Then, based on the singular perturbation method, the IGC problem is decomposed into the control design of the quasi-steady-state subsystem and the boundary-layer subsystem which can be designed separately. Finally, the receding horizon control is applied to the control design for the two subsystems. Simulation results show the effectiveness of the proposed approach.展开更多
弹药跌落环境模拟系统主要用于对各种弹药(箱装或裸弹)、引信、仪器设备等进行跌落试验。针对野外复杂背景下高速相机采集的目标跌落图像噪声大、边缘复杂不易提取且图像数据量大等问题,设计了融合高斯核函数和边窗思想的滤波算法、基...弹药跌落环境模拟系统主要用于对各种弹药(箱装或裸弹)、引信、仪器设备等进行跌落试验。针对野外复杂背景下高速相机采集的目标跌落图像噪声大、边缘复杂不易提取且图像数据量大等问题,设计了融合高斯核函数和边窗思想的滤波算法、基于感兴趣区域(region of interest,ROI)的改进Hough直线检测算法以及基于序列图像ROI动态更新的边缘直线自动提取算法,解决了去噪过程中目标边缘扩散和序列图像姿态角解算耗时长的问题。实验表明,所提出的改进算法保护了高噪声图像的边缘特征,直线检测耗时低于标准Hough变换耗时的1/10,实现了多帧图像运动目标姿态角的快速自动提取,姿态角解算平均绝对误差为0.36%。展开更多
文摘海洋一号C(HY-1C)卫星是中国首颗海洋水色业务卫星,其搭载的海岸带成像仪(Coastal Zone Imager, CZI)具有大幅宽、短重访周期的优势,可实现海洋和海岸带的大面积观测。作为光学传感器,CZI受云影响严重,准确识别云是CZI数据处理的关键,但是CZI缺少红外和短波红外等对云敏感的波段,云检测难度大。针对该问题,本文提出一种融合多尺度卷积和侧窗滤波的轻量化云检测方法,该方法通过多尺度卷积获取云的不同尺度特征,通过侧窗滤波突出边缘特征,减少椒盐噪声的影响,提升云边缘检测的精度。实验结果表明,本文所提出的方法可有效进行云检测,在云边缘提取方面表现较好,F1-score达92.77%,Kappa系数达0.89,与现有云检测方法相比优势明显,且模型训练速度快、参数量少,可为HY-1C CZI遥感影像处理提供有力支撑。
基金supported by National Natural Science Foundation of China (Nos. 61473099 and 61333001)
文摘This paper considers the guidance and control problem of a flight vehicle with sidewindow detection. In order to guarantee the target remaining in the seeker＇s sight of view, the line of sight and the attitude of the flight vehicle should be under some constraints caused by the sidewindow, which leads to coupling between the guidance and the attitude dynamics model. To deal with the side-window constraints and the coupling, a novel Integrated Guidance and Control（IGC）design approach is proposed. Firstly, the relative motion equations are derived in the body-Line of Sight（LOS） coordinate system. And the guidance and control problem of the flight vehicle is formulated into an IGC problem with state constraints. Then, based on the singular perturbation method, the IGC problem is decomposed into the control design of the quasi-steady-state subsystem and the boundary-layer subsystem which can be designed separately. Finally, the receding horizon control is applied to the control design for the two subsystems. Simulation results show the effectiveness of the proposed approach.
文摘弹药跌落环境模拟系统主要用于对各种弹药(箱装或裸弹)、引信、仪器设备等进行跌落试验。针对野外复杂背景下高速相机采集的目标跌落图像噪声大、边缘复杂不易提取且图像数据量大等问题,设计了融合高斯核函数和边窗思想的滤波算法、基于感兴趣区域(region of interest,ROI)的改进Hough直线检测算法以及基于序列图像ROI动态更新的边缘直线自动提取算法,解决了去噪过程中目标边缘扩散和序列图像姿态角解算耗时长的问题。实验表明,所提出的改进算法保护了高噪声图像的边缘特征,直线检测耗时低于标准Hough变换耗时的1/10,实现了多帧图像运动目标姿态角的快速自动提取,姿态角解算平均绝对误差为0.36%。
