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METHOD FOR PRODUCING THREE-DIMENSIONAL PICTURE SURFACE BASED ON BOARD pulse-Doppler radar low-altitude flight

机译:基于板载脉冲多普勒雷达低空飞行的三维图像表面制作方法

摘要

method u043fu043eu043bu0443u0447u0435u043du0438u00a0 3d u0438u0437u043eu0431u0440u0430u0436u0435u043du0438u00a0 surface in the zone of the radar u043cu0430u043bu043eu0432u044bu0441u043eu0442u043du043eu0433u043e flight u0437u0430u043au043bu044eu0447u0430u044eu0449u0438u0439u0441u00a0 in establishing the regime u043fu043eu0441u0442u0440u043eu0447u043du043eu0433u043e review contro u043bu0438u0440u0443u0435u043cu043eu0433u043e station space, combined with the u0443u0437u043au043eu043fu043eu043bu043eu0441u043du043eu0439 doppler filtering u043fu0440u0438u043du00a0u0442u044bu0445 signals u043fu043eu0437u0432u043eu043bu00a0u044eu0449u0435u0439 to cut u0440u0430u0437u0440u0435u0448u0435u043du0438 spatial elements u00a0 antenna into smaller pieces (u0434u043eu043fu043bu0435u0440u043eu0432u0441u043au0438u0435 elements u0440u0430u0437u0440u0435u0448u0435u043du0438u00a0 - der)and the formation of a three-dimensional matrix u0438u0437u043eu0431u0440u0430u0436u0435u043du0438u00a0 surface as the sum of reflected signal amplitude of der, and by rapid al u0435u043au0442u0440u043eu043du043du043eu0433u043e u043fu0435u0440u0435u043au043bu044eu0447u0435u043du0438u00a0 beam radar cause beam bearing and corner place of line by line on the width directional pattern antenna in the review and for each k, l, m u043fu043eu043bu043eu0436u0435u043du0438 and the beam bearing and corner seats u0438u0437u043cu0435u0440u00a0u044eu0442 amplitude signal a (i,(j) at the exit of the j th filter doppler frequencies in the 1 - m element u0440u0430u0437u0440u0435u0448u0435u043du0438u00a0 range thus obtained on a set of values i, j a two-dimensional image of the surface of the Akl (i, j) (,) in the k, l of the beam radar, u043eu0442u043bu0438u0447u0430u044eu0449u0438u0439u0441u00a0, u0434u043bu00a0 each measured with the l - m position of beam amplitude Akl (i, j), exceeding the threshold (the u043eu0431u043du0430u0440u0443u0436u0435u043du0438u00a0 reflection from the surface), choose a (i, j,k - e elements u043fu0440u00a0u043cu043eu0443u0433u043eu043bu044cu043du043eu0439 sampling grid, which coordinates (xi, u0443j, zk belong to the k, l, i, j of der, and border area are in advance by u043eu043fu0440u0435u0434u0435u043b u0435u043du043du043eu0439 methodology, and remember the Akl (i, j) in the matrix of amplitudes a (i, j), a maximum value of the third coordinates zk (height) in the matrix z (i, j), then u043fu043eu0432u0442u043eu0440u00a0u044eu0442 these opera all of the u0434u043bu00a0 kl - x of the beam and thereby form a three-dimensional image of the surface in the zone of the review in the form of a two-dimensional matrix a (i, j) and z (i, j), then u043fu0440u0438u0432u00a0u0437u044bu0432u0430u044eu0442 matrix to the current u0434u0438u0441u043au0440u0435u0442u043du043eu043cu0443 point of time t: a (i, j), z (i, j) and transmit them consistently points = 0, 1, 2,...the algorithms of space-time processing u0434u043bu00a0 u043fu043eu0432u044bu0448u0435u043du0438u00a0 quality images and algorithms u0434u043bu00a0 output images on screen display for the pilot.
机译:方法 u043f u043e u043b u0443 u0447 u0435 u043d u0438 u00a0 3d u0438 u0437 u043e u0431 u0440 u0430 u0436 u0435 u0435 u043d u0438 u00a0表面u043c u0430 u043b u043e u0432 u044b u0441 u043e u0442 u043d u043e u0433 u043e航班 u0437 u0430 u043a u043b u044e u0447 u0430 u044e u0449 u0438 u0439 u00a0建立体制 u043f u043e u0441 u0442 u0440 u043e u0447 u043d u043e u0433 u043e审查contro u043b u0438 u0440 u0443 u0435 u0435 u043c u043e u0433 u043e ,并与 u0443 u0437 u043a u043e u043f u043e u043b u043e u0441 u043d u043e u0439多普勒滤波 u043f u0440 u0438 u043d u00a0 u0442 u044b u0445信号 u043f u043e u0437 u0432 u043e u043b u00a0 u044e u0449 u0435 u0439切成 u0440 u0430 u0437 u0440 u0435 u0448 u0435 u043d u0438空间元素 u00a0天线成小块( u0434 u043e u043f u043b u0435 u0440 u043e u0432 u0441 u043a u0438 u0435元素 u0440 u0430 u0437 u0440 u0435 u0448 u0435 u0435 u043d u0438 u00a0- der)并形成三维矩阵 u0438 u0437 u043e u0431 u0440 u0430 u0436 u0435 u043d u0438 u00a0表面作为der反射信号幅度的总和,并通过快速al u0435 u043a u0442 u0440 u043e u043d u043d u043e u0433 u043e u043f u0435 u0440 u0435 u043a u043b u043b u044e u0447 u0435 u0435 u043d u043d u0438 u00a0光束原因在每个宽度,方向和方向图中,每个k,l,m的行数,以及每个波束轴承和角座 u0438 u0437 u043c u0435 u0440 u00a0 u044e u0442在1-m元素 u0440 u0430 u0437 u0440 u0435 u0448 u0435 中第j个滤波器多普勒频率的出口处的振幅信号a(i,(j)这样就在一组值i,ja上获得了范围,该值i,ja是波束雷达的k,l中的Akl(i,j)(,)表面的二维图像, u043e u0442 u043b u0438 u0447 u0430 u044e u0449 u0438 u0439 u0441 u00a0, u0434 u043b u00a0每个红色,且光束振幅Akl(i,j)的l-m位置超过阈值( u043e u0431 u043d u0430 u0440 u0443 u0436 u0435 u043d u0438 u00a0从表面反射),选择一个(i,j,k-e元素 u043f u0440 u00a0 u043c u043e u0443 u0433 u043e u043b u044c u043d u043e u0439采样网格,其坐标(xi, u0443j,zk属于通过 u043e u043f u0440 u0435 u0434 u0435 u043b u0435 u043d u043d u043d u043e u0439方法预先确定der的k,l,i,j和边界区域i,j)在幅度矩阵a(i,j)中,矩阵z(i,j)中第三坐标zk(高度)的最大值,则 u043f u043e u0432 u0442 u043e u0440 u00a0 u044e u0442这些操作操作了光束的所有 u0434 u043b u00a0 kl-x,从而以二维矩阵a的形式在检查区域中形成了表面的三维图像。 (i,j)和z(i,j),则 u043f u0440 u0438 u0432 u00a0 u0437 u044b u0432 u0430 u044e u0442矩阵t u0434 u0438 u0441 u043a u0440 u0435 u0442 u043d u043e u043c u0443时间点t:a(i,j),z(i,j)并始终一致地发送它们= 0,1 ,2,...时空处理算法 u0434 u043b u00a0 u043f u043e u0432 u044b u0448 u0435 u043d u0438 u00a0质量图像和算法 u0434 u043b u00a0输出图像飞行员的屏幕显示。

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