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CN107818697B - Non-horizontal route design method based on terrain elevation, terminal and storage medium - Google Patents

Non-horizontal route design method based on terrain elevation, terminal and storage medium Download PDF

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CN107818697B
CN107818697B CN201711039413.0A CN201711039413A CN107818697B CN 107818697 B CN107818697 B CN 107818697B CN 201711039413 A CN201711039413 A CN 201711039413A CN 107818697 B CN107818697 B CN 107818697B
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CN107818697A (en
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赵海涛
黎东
左正立
陶斯倩
张兵
陈正超
吴亮
谭骏翔
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Institute of Remote Sensing and Digital Earth of CAS
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Abstract

本发明提供了基于地形高程的非水平航线设计方法,包括:基于采样的地形高,自动拟合航线上的各个非水平航段;基于共线方程数学模型计算起算航线和初始邻近航线的地面覆盖范围,从而求出两者的重叠度,调整初始邻近航线的位置,使其自适应的达到设计重叠度的要求。基于上述基于地形高程的非水平航线设计方法,本发明还提供了一种终端及存储介质。利用本发明的技术方案,能够基于地形高自动计算非水平航线,以保证航线上各采样点的相对航高差值在规定的阈值内,从而能够获得更好的遥感飞行监测效果。

Figure 201711039413

The invention provides a method for designing a non-horizontal route based on terrain elevation, including: automatically fitting each non-horizontal flight segment on the route based on the sampled terrain height; calculating the ground coverage of the starting route and the initial adjacent route based on a collinear equation mathematical model range, so as to obtain the overlap degree of the two, and adjust the position of the initial adjacent route so that it can adaptively meet the requirements of the design overlap degree. Based on the above-mentioned non-horizontal route design method based on terrain elevation, the present invention also provides a terminal and a storage medium. Using the technical solution of the present invention, the non-horizontal route can be automatically calculated based on the terrain height, so as to ensure that the relative altitude difference of each sampling point on the route is within a specified threshold, so that a better remote sensing flight monitoring effect can be obtained.

Figure 201711039413

Description

基于地形高程的非水平航线设计方法、终端及存储介质Non-horizontal route design method, terminal and storage medium based on terrain elevation

技术领域technical field

本发明涉及航空遥感领域,特别涉及一种基于地形高程的非水平航线设计方法、终端及存储介质。The invention relates to the field of aerial remote sensing, in particular to a non-horizontal route design method, terminal and storage medium based on terrain elevation.

背景技术Background technique

传统航空遥感航线设计时,考虑到固定翼飞机飞行导航的便捷性和安全性,航线设计时,各个航线的航线起点和终点绝对航高是相同的,即保持飞机平飞;如今随着旋翼飞机用于航空遥感,其飞行时可以保持非水平飞行,且为获得分辨率一致的影像数据及激光点云数据,需要保持相对航高的一致性;同时对于航空物探遥感,为获得较好的遥感探测效果,也需要保持相对航高一致的起伏飞行,但是目前在地形起伏区域,传统的手工航线设计非常不便。In the design of traditional aviation remote sensing routes, taking into account the convenience and safety of fixed-wing aircraft flight navigation, the absolute altitudes of the starting and ending points of each route are the same, that is, to keep the aircraft in level flight; For aerial remote sensing, it can maintain non-level flight during flight, and in order to obtain image data and laser point cloud data with consistent resolution, it is necessary to maintain the consistency of relative altitude; meanwhile, for aerial geophysical remote sensing, in order to obtain better remote sensing The detection effect also needs to maintain a undulating flight with a consistent relative altitude, but currently in the terrain undulating area, the traditional manual route design is very inconvenient.

发明内容SUMMARY OF THE INVENTION

为了适应地形起伏区域的航线设计要求,本发明提供了一种基于地形高程的非水平航线设计方法、终端及存储介质。In order to meet the route design requirements of terrain undulating areas, the present invention provides a non-horizontal route design method, terminal and storage medium based on terrain elevation.

本发明提供的基于地形高程的非水平航线设计方法,包括以下步骤:确定待测区域内的起算航线,基于预设的采样间距在所述起算航线上采集若干个采样点;将每一个采样点对应的地面点加上预设的相对航高变换为空中点,所有空中点按顺序排列形成空中点集,将所述空中点集通过线性回归进行线段拟合,得到所述起算航线对应的非水平航线,其中所述非水平航线由多个连续的线段组成;以所述起算航线作为参考航线,根据预设的旁向间距得到邻近航线,将所述邻近航线对应的空中点集通过线性回归进行线段拟合得到所述邻近航线对应的非水平航线;计算参考航线对应的非水平航线与所述邻近航线对应的非水平航线的重叠度,当所述重叠度满足预设的条件时,所述邻近航线对应的非水平航线即为所述待测区域内的下一条非水平航线;以所述计算出的邻近航线作为参考航线,继续敷设非水平航线,直到敷设的当前非水平航线的旁向方向坐标值不位于所述待测区域旁向方向的最大坐标值和最小坐标值之间时,停止航敷设。The method for designing a non-horizontal route based on terrain elevation provided by the present invention includes the following steps: determining a starting route in the area to be measured, collecting several sampling points on the starting route based on a preset sampling interval; The corresponding ground point plus the preset relative altitude is transformed into an air point, all the air points are arranged in order to form an air point set, and the air point set is subjected to line segment fitting through linear regression, and the non-linear corresponding to the starting route is obtained. A horizontal route, wherein the non-horizontal route is composed of a plurality of continuous line segments; the starting route is used as a reference route, the adjacent route is obtained according to the preset lateral distance, and the air point set corresponding to the adjacent route is passed through linear regression Perform line segment fitting to obtain the non-horizontal air route corresponding to the adjacent air route; calculate the degree of overlap between the non-horizontal air route corresponding to the reference air route and the non-horizontal air route corresponding to the adjacent air route. The non-horizontal route corresponding to the adjacent route is the next non-horizontal route in the area to be tested; with the calculated adjacent route as the reference route, continue to lay the non-horizontal route until the side of the current non-horizontal route being laid. When the coordinate value of the lateral direction is not between the maximum coordinate value and the minimum coordinate value of the lateral direction of the area to be measured, the aerial installation is stopped.

具体的,在本发明所述的基于地形高程的非水平航线设计方法中,确定待测区域内的起算航线,包括:基于航线设计方向,将起算航线的Y值设置为(Ymin+Ymax)/2,获取所述起算航线与所述待测区域的交点,以确定所述起算航线的起点坐标和终点坐标;其中Ymin为所述待测区域角点的最小Y值坐标,Ymax为所述待测区域角点的最大Y值坐标。Specifically, in the non-horizontal route design method based on terrain elevation according to the present invention, determining the starting route in the area to be measured includes: setting the Y value of the starting route to (Y min +Y max based on the route design direction) )/2, obtain the intersection point of the starting route and the area to be measured, to determine the coordinates of the starting point and the end point of the starting route; wherein Y min is the minimum Y value coordinate of the corner point of the area to be measured, and Y max is the maximum Y value coordinate of the corner point of the area to be measured.

具体的,在本发明所述的基于地形高程的非水平航线设计方法中,将所述空中点集通过线性回归进行线段拟合,得到所述起算航线对应的非水平航线,包括:以所述空中点集的起点作为起点将所述空中点集进行线段拟合,当所述空中点集中参与拟合的点到拟合出的线段的高程差值大于预先设定的阈值时,停止拟合,得到第一航段;以所述第一航段作为当前航段,以所述当前航段的终点作为起点继续将剩余的空中点集进行线段拟合,当所述空中点集中参与拟合的点到拟合出的线段的高程差值大于预先设定的阈值时,停止拟合,得到下一航段;以所述下一航段作为当前航段继续进行线段拟合,直到所述空中点集中的空中点全部拟合完毕,得到所述起算航线对应的非水平航线。Specifically, in the method for designing a non-horizontal route based on terrain elevation of the present invention, performing line segment fitting on the air point set through linear regression to obtain a non-horizontal route corresponding to the starting route, including: using the The starting point of the aerial point set is used as the starting point to perform line segment fitting on the aerial point set. When the difference in elevation between the points participating in the fitting in the aerial point set and the fitted line segment is greater than a preset threshold, the fitting is stopped. , to obtain the first flight segment; take the first flight segment as the current flight segment, and use the end point of the current flight segment as the starting point to continue to perform line segment fitting on the remaining air point set, when the air point set participates in the fitting When the difference in elevation between the point and the fitted line segment is greater than the preset threshold, the fitting is stopped and the next segment is obtained; the next segment is used as the current segment and the line segment fitting is continued until the After all the air points in the air point set are fitted, the non-horizontal route corresponding to the starting route is obtained.

具体的,在本发明所述的基于地形高程的非水平航线设计方法中,以所述起算航线作为参考航线,根据预设的旁向间距得到邻近航线,包括:以所述起算航线作为参考航线,利用所述参考航线的Y坐标加上或减去预设的旁向间距,得到邻近航线的Y坐标;基于航线设计方向和所述邻近航线的Y坐标,获取所述邻近航线与所述待测区域的交点,以确定所述邻近航线的起点坐标和终点坐标,得到邻近航线。Specifically, in the method for designing a non-horizontal route based on terrain elevation according to the present invention, the starting route is used as a reference route, and adjacent routes are obtained according to a preset lateral spacing, including: using the starting route as a reference route , use the Y coordinate of the reference route to add or subtract the preset lateral distance to obtain the Y coordinate of the adjacent route; based on the route design direction and the Y coordinate of the adjacent route, obtain the adjacent route and the pending route. The intersection point of the survey area is determined to determine the coordinates of the start point and the end point of the adjacent route to obtain the adjacent route.

具体的,在本发明所述的基于地形高程的非水平航线设计方法中,计算参考航线对应的非水平航线与所述邻近航线对应的非水平航线的重叠度,当所述重叠度满足预设的条件时,所述邻近航线对应的非水平航线即为所述待测区域内的下一条非水平航线,包括:利用共线方程数学模型计算所述邻近航线对应的非水平航线的地面覆盖范围;利用共线方程数学模型计算所述参考航线对应的非水平航线的地面覆盖范围;获取上述两个地面覆盖范围的交集多边形在Y方向的最窄距离,所述最窄距离除以基准面旁向幅宽得到最小重叠度;计算所述最小重叠度与理论重叠度的差值,当所述差值满足预设的阈值时,所述邻近航线对应的非水平航线即为即为所述待测区域内的下一条非水平航线。Specifically, in the method for designing a non-horizontal air route based on terrain elevation according to the present invention, the degree of overlap between the non-horizontal air route corresponding to the reference air route and the non-horizontal air route corresponding to the adjacent air route is calculated. When the conditions are met, the non-horizontal air route corresponding to the adjacent air route is the next non-horizontal air route in the area to be tested, including: calculating the ground coverage of the non-horizontal air route corresponding to the adjacent air route by using a collinear equation mathematical model ; Calculate the ground coverage of the non-horizontal route corresponding to the reference route using the mathematical model of the collinear equation; Obtain the narrowest distance in the Y direction of the intersection polygon of the above-mentioned two ground coverages, and divide the narrowest distance by the side of the reference plane. The minimum overlap degree is obtained from the width; the difference between the minimum overlap degree and the theoretical overlap degree is calculated. When the difference satisfies the preset threshold, the non-horizontal air route corresponding to the adjacent air route is the The next non-horizontal route within the survey area.

具体的,在本发明所述的基于地形高程的非水平航线设计方法中,还包括:当所述重叠度不满足预设的条件时,计算所述邻近航线Y坐标的调整量;根据所述邻近航线Y坐标的调整量调整所述邻近航线的Y坐标,并重新求得调整后的邻近航向的起点坐标和终点坐标,及进行非水平航线拟合和重叠度计算,直到当重新计算的重叠度满足预设的条件。Specifically, in the method for designing a non-horizontal route based on terrain elevation according to the present invention, the method further includes: when the overlapping degree does not meet a preset condition, calculating the adjustment amount of the Y coordinate of the adjacent route; according to the The adjustment amount of the Y coordinate of the adjacent route adjusts the Y coordinate of the adjacent route, and re-obtains the start and end coordinates of the adjusted adjacent route, and performs non-horizontal route fitting and overlap calculation until the recalculated overlap meet the preset conditions.

具体的,在本发明所述的基于地形高程的非水平航线设计方法中,在确定起算航线的位置之前,还包括:根据航线敷设方向进行坐标系旋转,以使得旋转后坐标系的X轴平行于敷设的航线;确定航线方向为坐标系的X轴,以及确定航线的旁向方向为坐标系的Y轴。Specifically, in the non-horizontal route design method based on terrain elevation according to the present invention, before determining the position of the starting route, the method further includes: rotating the coordinate system according to the route laying direction, so that the X axis of the rotated coordinate system is parallel Determine the route direction as the X axis of the coordinate system, and determine the side direction of the route as the Y axis of the coordinate system.

具体的,在本发明所述的基于地形高程的非水平航线设计方法中,在停止航线敷设之后,还包括:进行坐标系反变换,重新确定新的航线坐标,以将航线坐标变换为地图投影坐标系下的坐标。Specifically, in the method for designing a non-horizontal route based on terrain elevation according to the present invention, after stopping the laying of the route, the method further includes: performing an inverse transformation of the coordinate system, and re-determining the coordinates of the new route, so as to transform the route coordinates into a map projection The coordinates in the coordinate system.

本发明还提供了一种终端,所述终端包括:存储器、处理器及存储在所述存储器上并可在所述处理器上运行的计算机程序,所述计算机程序被所述处理器执行时实现如上所述的基于地形高程的非水平航线设计方法的步骤。The present invention also provides a terminal, which includes: a memory, a processor, and a computer program stored on the memory and running on the processor, and the computer program is implemented when executed by the processor The steps of the method for designing a non-horizontal route based on terrain elevation as described above.

本发明还提供了一种存储介质,所述存储介质上存储有基于地形高程的非水平航线设计程序,所述基于地形高程的非水平航线设计程序被处理器执行时实现如上所述的基于地形高程的非水平航线设计方法的步骤。所述存储介质为计算机可读存储介质。The present invention also provides a storage medium on which a terrain-elevation-based non-horizontal route design program is stored, and the terrain-elevation-based non-horizontal route design program is executed by a processor to realize the above-mentioned terrain-based route design program Steps of a method for designing a non-horizontal route of elevation. The storage medium is a computer-readable storage medium.

本发明的有益效果如下:The beneficial effects of the present invention are as follows:

本发明实施例提供的基于地形高程的非水平航线设计方法、终端及存储介质,能够基于地形高自动计算非水平航线,从而保证航线上各采样点的相对航高差值在规定的阈值内,从而能够获得更好的遥感飞行监测效果。The terrain elevation-based non-horizontal route design method, terminal, and storage medium provided by the embodiments of the present invention can automatically calculate the non-horizontal route based on the terrain elevation, thereby ensuring that the relative altitude difference of each sampling point on the route is within a specified threshold, Thus, a better remote sensing flight monitoring effect can be obtained.

附图说明Description of drawings

图1是本发明方法实施例的基于地形高程的非水平航线设计方法的流程图;Fig. 1 is the flow chart of the non-horizontal route design method based on terrain elevation of the method embodiment of the present invention;

图2是本发明方法实施例中起算航线对应的非水平航线的设计效果示意图;Fig. 2 is the design effect schematic diagram of the non-horizontal route corresponding to the starting route in the method embodiment of the present invention;

图3是本发明方法实施例中两邻近航线的地面覆盖范围的交集多边形在Y方向的最窄距离的示意图;3 is a schematic diagram of the narrowest distance in the Y direction of the intersection polygon of the ground coverage of two adjacent air routes in an embodiment of the method of the present invention;

图4是实例1中基于地形高程的非水平航线设计方法的流程示意图;Fig. 4 is the schematic flow chart of the non-horizontal route design method based on terrain elevation in example 1;

图5是实例1中自适应计算航线上各个航段的流程示意图;Fig. 5 is the schematic flow chart of each flight segment on the self-adaptive calculation route in example 1;

图6是实例1中自适应计算邻近待求航线对应的非水平航线的流程示意图;6 is a schematic flowchart of adaptive calculation of the non-horizontal route corresponding to the adjacent route to be sought in Example 1;

图7是实例1中基于地形高程的非水平航线的航线设计结果的倾斜视图;7 is an oblique view of route design results for a non-horizontal route based on terrain elevation in Example 1;

图8是实例1中基于地形高程的非水平航线的航线设计结果的俯视图。FIG. 8 is a top view of the route design result of the terrain elevation-based non-horizontal route in Example 1. FIG.

具体实施方式Detailed ways

下面将参照附图更详细地描述本公开的示例性实施例。虽然附图中显示了本公开的示例性实施例,然而应当理解,可以以各种形式实现本公开而不应被这里阐述的实施例所限制。相反,提供这些实施例是为了能够更透彻地理解本公开,并且能够将本公开的范围完整的传达给本领域的技术人员。Exemplary embodiments of the present disclosure will be described in more detail below with reference to the accompanying drawings. While exemplary embodiments of the present disclosure are shown in the drawings, it should be understood that the present disclosure may be embodied in various forms and should not be limited by the embodiments set forth herein. Rather, these embodiments are provided so that the present disclosure will be more thoroughly understood, and will fully convey the scope of the present disclosure to those skilled in the art.

为了适应地形起伏区域的航线设计要求,本发明提供了一种基于地形高程的非水平航线设计方法、终端及存储介质,以下结合附图对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅仅用以解释本发明,并不限定本发明。In order to meet the requirements of route design in terrain undulating areas, the present invention provides a non-horizontal route design method, terminal and storage medium based on terrain elevation. The present invention will be further described in detail below with reference to the accompanying drawings. It should be understood that the specific embodiments described herein are only used to illustrate the present invention, but not to limit the present invention.

根据本发明的方法实施例,提供了一种基于地形高程的非水平航线设计方法,图1是本发明方法实施例的基于地形高程的非水平航线设计方法的流程图,如图1所示,本发明方法实施例的基于地形高程的非水平航线设计方法,包括以下步骤:According to an embodiment of the method of the present invention, a method for designing a non-horizontal route based on terrain elevation is provided. FIG. 1 is a flowchart of a method for designing a non-horizontal route based on terrain elevation according to an embodiment of the method of the present invention, as shown in FIG. 1 , The non-horizontal route design method based on terrain elevation according to the method embodiment of the present invention includes the following steps:

S101:确定待测区域内的起算航线,基于预设的采样间距在所述起算航线上采集若干个采样点。S101: Determine a starting route in the area to be measured, and collect several sampling points on the starting route based on a preset sampling interval.

具体的,确定待测区域内的起算航线,包括:基于航线设计方向,将起算航线的Y值设置为(Ymin+Ymax)/2,获取所述起算航线与所述待测区域的交点,以确定所述起算航线的起点坐标和终点坐标;其中Ymin为所述待测区域角点的最小Y值坐标,Ymax为所述待测区域角点的最大Y值坐标。Specifically, determining the starting route in the area to be measured includes: based on the route design direction, setting the Y value of the starting route to (Y min + Y max )/2, and obtaining the intersection of the starting route and the area to be measured , to determine the start and end coordinates of the starting route; wherein Y min is the minimum Y value coordinate of the corner point of the area to be measured, and Y max is the maximum Y value coordinate of the corner point of the area to be measured.

S102:将每一个采样点对应的地面点加上预设的相对航高变换为空中点,所有空中点按顺序排列形成空中点集,将所述空中点集通过线性回归进行线段拟合,得到所述起算航线对应的非水平航线,其中所述非水平航线由多个连续的线段组成。S102: Transform the ground point corresponding to each sampling point plus a preset relative altitude into an air point, arrange all the air points in sequence to form an air point set, and perform line segment fitting on the air point set through linear regression to obtain The non-horizontal route corresponding to the starting route, wherein the non-horizontal route is composed of a plurality of continuous line segments.

具体的,将所述空中点集通过线性回归进行线段拟合,得到所述起算航线对应的非水平航线,包括:以所述空中点集的起点作为起点将所述空中点集进行线段拟合,当所述空中点集中参与拟合的点到拟合出的线段的高程差值大于预先设定的阈值时,停止拟合,得到第一航段;以所述第一航段作为当前航段,以所述当前航段的终点作为起点继续将剩余的空中点集进行线段拟合,当所述空中点集中参与拟合的点到拟合出的线段的高程差值大于预先设定的阈值时,停止拟合,得到下一航段;以所述下一航段作为当前航段继续进行后续的线段拟合,直到所述空中点集中的空中点全部拟合完毕,得到所述起算航线对应的非水平航线。图2是本发明方法实施例中起算航线对应的非水平航线的设计效果示意图,在图2中,上面的一条折线为起算航线对应的非水平航线;下面一条弯曲曲线为起算航线对应的地形高程截面。Specifically, performing line segment fitting on the aerial point set through linear regression to obtain a non-horizontal route corresponding to the starting route includes: using the starting point of the aerial point set as a starting point to perform line segment fitting on the aerial point set , when the height difference between the points participating in the fitting in the air point set and the fitted line segment is greater than the preset threshold, stop the fitting and obtain the first flight segment; take the first flight segment as the current flight segment segment, using the end point of the current flight segment as the starting point to continue to perform line segment fitting on the remaining air point set, when the height difference between the points participating in the fitting in the air point set and the fitted line segment is greater than the preset value When the threshold is reached, the fitting is stopped to obtain the next flight segment; the next flight segment is used as the current flight segment to continue the subsequent line segment fitting until all the air points in the air point set are fitted, and the starting calculation is obtained. The non-horizontal route corresponding to the route. Fig. 2 is a schematic diagram of the design effect of the non-horizontal route corresponding to the starting route in the embodiment of the method of the present invention. In Fig. 2, the upper broken line is the non-horizontal route corresponding to the starting route; the lower curved curve is the terrain elevation corresponding to the starting route. section.

S103:以所述起算航线作为参考航线,根据预设的旁向间距得到邻近航线,将所述邻近航线对应的空中点集通过线性回归进行线段拟合得到所述邻近航线对应的非水平航线。S103: Using the starting route as a reference route, obtain an adjacent route according to a preset lateral distance, and perform line segment fitting on the air point set corresponding to the adjacent route through linear regression to obtain a non-horizontal route corresponding to the adjacent route.

具体的,以所述起算航线作为参考航线,根据预设的旁向间距得到邻近航线,包括:以所述起算航线作为参考航线,利用所述参考航线的Y坐标加上或减去预设的旁向间距,得到邻近航线的Y坐标;基于航线设计方向和所述邻近航线的Y坐标,获取所述邻近航线与所述待测区域的交点,以确定所述邻近航线的起点坐标和终点坐标,得到邻近航线。Specifically, taking the starting route as a reference route, and obtaining adjacent routes according to a preset lateral distance, including: taking the starting route as a reference route, and using the Y coordinate of the reference route to add or subtract a preset route The lateral distance is used to obtain the Y coordinate of the adjacent air route; based on the route design direction and the Y coordinate of the adjacent air route, the intersection point of the adjacent air route and the area to be measured is obtained to determine the start and end coordinates of the adjacent air route. , get the adjacent route.

S104:计算参考航线对应的非水平航线与所述邻近航线对应的非水平航线的重叠度,当所述重叠度满足预设的条件时,所述邻近航线对应的非水平航线即为所述待测区域内的下一条非水平航线。S104: Calculate the degree of overlap between the non-horizontal air route corresponding to the reference air route and the non-horizontal air route corresponding to the adjacent air route. When the degree of overlap satisfies a preset condition, the non-horizontal air route corresponding to the adjacent air route is the non-horizontal air route corresponding to the adjacent air route. The next non-horizontal route within the survey area.

具体的,计算参考航线对应的非水平航线与所述邻近航线对应的非水平航线的重叠度,当所述重叠度满足预设的条件时,所述邻近航线对应的非水平航线即为所述待测区域内的下一条非水平航线,包括:利用共线方程数学模型计算所述邻近航线对应的非水平航线的地面覆盖范围;利用共线方程数学模型计算所述参考航线对应的非水平航线的地面覆盖范围;获取上述两个地面覆盖范围的交集多边形在Y方向的最窄距离,所述最窄距离除以基准面旁向幅宽得到最小重叠度;计算所述最小重叠度与理论重叠度的差值,当所述差值满足预设的阈值时,所述邻近航线对应的非水平航线即为即为所述待测区域内的下一条非水平航线。图3是本发明方法实施例中两邻近航线的地面覆盖范围的交集多边形在Y方向的最窄距离的示意图。具体的,获取所述参考航线对应的非水平航线的地面覆盖范围与所述邻近航线对应的非水平航线的地面覆盖范围的交集多边形在Y方向的最窄距离QY-MIN,所述最窄距离除以LY得到最小重叠度,其中LY为所述预设的相对航高下对应的地面旁向幅宽(基准面旁向幅宽),LY=2H*tan(θ/2),H为相对航高,θ为航空遥感传感器的旁向视场角。Specifically, the degree of overlap between the non-horizontal air route corresponding to the reference air route and the non-horizontal air route corresponding to the adjacent air route is calculated. When the degree of overlap satisfies a preset condition, the non-horizontal air route corresponding to the adjacent air route is the non-horizontal air route corresponding to the adjacent air route. The next non-horizontal route in the area to be tested includes: calculating the ground coverage of the non-horizontal route corresponding to the adjacent route by using a collinear equation mathematical model; calculating the non-horizontal route corresponding to the reference route by using the collinear equation mathematical model obtain the narrowest distance in the Y direction of the intersection polygon of the above two ground coverages, and divide the narrowest distance by the lateral width of the reference plane to obtain the minimum overlap; calculate the minimum overlap and the theoretical overlap When the difference meets a preset threshold, the non-horizontal route corresponding to the adjacent route is the next non-horizontal route in the area to be measured. 3 is a schematic diagram of the narrowest distance in the Y direction of the intersection polygon of the ground coverage areas of two adjacent air routes in an embodiment of the method of the present invention. Specifically, obtain the narrowest distance Q Y-MIN in the Y direction of the intersection polygon of the ground coverage of the non-horizontal air route corresponding to the reference air route and the ground coverage of the non-horizontal air route corresponding to the adjacent air route. The minimum overlap is obtained by dividing the distance by L Y , where L Y is the corresponding ground lateral width (reference plane lateral width) under the preset relative flight height, L Y =2H*tan(θ/2) , H is the relative flight height, and θ is the lateral field of view of the aerial remote sensing sensor.

本发明提供的基于地形高程的非水平航线设计方法,还包括以下步骤:当所述重叠度不满足预设的条件时,计算所述邻近航线Y坐标的调整量;根据所述邻近航线Y坐标的调整量调整所述邻近航线的Y坐标,并重新求得调整后的邻近航向的起点坐标和终点坐标,及进行非水平航线拟合和重叠度计算,直到当重新计算的重叠度满足预设的条件。具体的,所述邻近航线Y坐标的调整量=(QY-MIN-QY-PLAN)*LY,其中,QY-PLAN为理论重叠度。The method for designing a non-horizontal air route based on terrain elevation provided by the present invention further includes the following steps: when the overlapping degree does not meet a preset condition, calculating the adjustment amount of the Y coordinate of the adjacent air route; according to the Y coordinate of the adjacent air route Adjust the Y coordinate of the adjacent route by the adjustment amount, and re-obtain the start and end coordinates of the adjusted adjacent route, and perform non-horizontal route fitting and overlap calculation until the recalculated overlap meets the preset conditions of. Specifically, the adjustment amount of the Y coordinate of the adjacent air route=(Q Y-MIN -Q Y-PLAN )*L Y , where Q Y-PLAN is the theoretical overlap degree.

S105:以所述邻近航线作为新的参考航线,继续敷设非水平航线,直到敷设的当前非水平航线的旁向方向坐标值不位于所述待测区域旁向方向的最大坐标值和最小坐标值之间时,停止航线敷设。S105: Using the adjacent route as a new reference route, continue to lay the non-horizontal route until the lateral direction coordinate value of the current non-horizontal route being laid is not located at the maximum coordinate value and the minimum coordinate value of the lateral direction of the area to be measured In between, stop the route laying.

本发明提供的基于地形高程的非水平航线设计方法,在确定起算航线的位置之前,还包括以下步骤:根据航线敷设方向进行坐标系旋转,以使得旋转后坐标系的X轴平行于敷设的航线;确定航线方向为坐标系的X轴,以及确定航线的旁向方向为坐标系的Y轴。The method for designing a non-horizontal route based on terrain elevation provided by the present invention further includes the following steps before determining the position of the starting route: rotating the coordinate system according to the route laying direction, so that the X-axis of the rotated coordinate system is parallel to the route to be laid ; Determine the route direction as the X axis of the coordinate system, and determine the side direction of the route as the Y axis of the coordinate system.

本发明提供的基于地形高程的非水平航线设计方法,在停止航线敷设之后,还包括以下步骤:进行坐标系反变换,重新确定新的航线坐标,以将航线坐标变换为地图投影坐标系下的坐标。The method for designing a non-horizontal route based on terrain elevation provided by the present invention further includes the following steps after the route laying is stopped: inverse transformation of the coordinate system is performed, and new route coordinates are re-determined, so as to transform the route coordinates into the map projection coordinate system. coordinate.

为了更加详细的说明本发明方法实施例的基于地形高程的非水平航线设计方法,给出实例1。Example 1 is given in order to illustrate the non-horizontal route design method based on terrain elevation in the method embodiment of the present invention in more detail.

实例1中基于地形高程的非水平航线设计方法包括以下步骤:首先根据待测区域的范围,确定起算航线的位置,而后计算该航线上按一定水平间距取样的点对应的地面点;将此所有的地面点加上相对航高,形成空中的点集,将此点集进行分段拟合,拟合为连续的折线线段;拟合折线的跳出条件为以点集中参与拟合的点到该拟合折线的高程差值大于阈值时则该线段为所求的拟合线段;以此拟合线段的终点为下一个拟合线段的起点,重新拟合下一个线段,同理判断点集中参与拟合的点,到该拟合线段的高程距离,当高程距离大于阈值时停止拟合;依次类推,确定该航线上所有其他的航线折线线段,从而完成本条航线的其他折线线段的自动设计;同理按照预设的旁向间距确定其邻近的待求航线的初始位置,依据上述步骤,拟合出此航线上的连续的折线航段,将待求航线折线航段和参考航线依据地面范围的覆盖关系求解最小重叠度,当最小重叠度小于预设重叠度时待求航线向远离参考航线方向移动,当最小重叠度大于预设重叠度时待求航线向靠近参考航线方向移动,反复进行此过程,直到重叠度在规定的阈值内时停止,即求解出待求航线;以上一个的待求航线为新的参考航线,按照上述步骤,求解下一个待求航线,根据待测区域的范围作为限制条件,依次即可完成所有航线的自适应航线设计。图4是实例1中基于地形高程的非水平航线设计方法的设计总流程图;图5是实例1中自适应计算航线上各个航段的流程示意图;图6是实例1中自适应计算邻近待求航线对应的非水平航线的流程示意图。The non-horizontal route design method based on terrain elevation in Example 1 includes the following steps: first, according to the range of the area to be measured, determine the position of the starting route, and then calculate the ground points corresponding to the points sampled at a certain horizontal interval on the route; The ground points of , plus the relative altitude, form a point set in the air, and this point set is segmented and fitted to a continuous polyline segment. When the height difference of the fitted polyline is greater than the threshold, the line segment is the desired fitted line segment; the end point of the fitted line segment is the starting point of the next fitted line segment, and the next line segment is re-fitted. Fitted point, the elevation distance to the fitted line segment, when the elevation distance is greater than the threshold, stop fitting; and so on, determine all other route polyline segments on the route, so as to complete the automatic design of other polyline segments of this route; Similarly, the initial position of the adjacent route to be sought is determined according to the preset lateral distance, and according to the above steps, the continuous broken-line segment on this route is fitted, and the broken-line segment of the route to be sought and the reference route are based on the ground range. When the minimum overlap is less than the preset overlap, the route to be sought moves away from the reference route, and when the minimum overlap is greater than the preset overlap, the route to be sought moves closer to the reference route, and repeats This process stops when the overlap degree is within the specified threshold, that is, the route to be sought is solved; the previous route to be sought is the new reference route, and the next route to be sought is solved according to the above steps, according to the scope of the area to be measured. As a constraint, the adaptive route design of all routes can be completed in sequence. Fig. 4 is the design general flow chart of the non-horizontal route design method based on terrain elevation in the example 1; Fig. 5 is the schematic flow chart of each flight segment on the self-adaptive calculation route in the example 1; Fig. 6 is the self-adaptive calculation adjacent to the example 1 A schematic diagram of the process of finding the non-horizontal route corresponding to the route.

图7是实例1中基于地形高程的非水平航线的航线设计结果的倾斜视图,在图7中,测区由14条航线构成,有些航线有多个航段组成,根据地形起伏自动调整。图8是实例1中基于地形高程的非水平航线的航线设计结果的俯视图(即将图7的观察视角变成垂直向下),如图8所示,测区由14条航线构成,可以看到航线上各个航段在一条直线上。Figure 7 is an oblique view of the route design result of the non-horizontal route based on terrain elevation in Example 1. In Figure 7, the survey area consists of 14 routes, and some routes consist of multiple segments, which are automatically adjusted according to terrain fluctuations. Fig. 8 is a top view of the route design result of the non-horizontal route based on terrain elevation in Example 1 (that is, the viewing angle of Fig. 7 becomes vertically downward). As shown in Fig. 8, the survey area is composed of 14 routes, and it can be seen that Each segment on the route is in a straight line.

本发明还提供了一种终端,所述终端包括:存储器、处理器及存储在所述存储器上并可在所述处理器上运行的计算机程序,所述计算机程序被所述处理器执行时实现如上所述的基于地形高程的非水平航线设计方法的步骤。The present invention also provides a terminal, which includes: a memory, a processor, and a computer program stored on the memory and running on the processor, and the computer program is implemented when executed by the processor The steps of the method for designing a non-horizontal route based on terrain elevation as described above.

本发明还提供了一种存储介质,所述存储介质上存储有基于地形高程的非水平航线设计程序,所述基于地形高程的非水平航线设计程序被处理器执行时实现如上所述的基于地形高程的非水平航线设计方法的步骤。The present invention also provides a storage medium on which a terrain-elevation-based non-horizontal route design program is stored, and the terrain-elevation-based non-horizontal route design program is executed by a processor to realize the above-mentioned terrain-based route design program Steps of a method for designing a non-horizontal route of elevation.

本发明实施例通过地形高程数据(DEM),基于采样的地形高,自动拟合航线上的各个非水平航段;基于共线方程数学模型计算起算航线和初始邻近航线的地面覆盖范围,从而求出两者的重叠度,调整初始邻近航线的位置,使其自适应的达到设计重叠度的要求。与现有技术相比本发明具有以下优点:1.The embodiment of the present invention uses the terrain elevation data (DEM) to automatically fit each non-horizontal flight segment on the route based on the sampled terrain height; To find out the overlap between the two, adjust the position of the initial adjacent route so that it can adaptively meet the requirements of the design overlap. Compared with the prior art, the present invention has the following advantages: 1.

能够基于地形数据计算非水平航线,从而在飞行设计阶段能够保证航空遥感数据获取质量;2.基于地形数据全自动的计算飞行航线,减少以前人工非水平航线设计的工作量。It can calculate non-horizontal routes based on terrain data, so as to ensure the quality of aerial remote sensing data acquisition in the flight design stage; 2. Automatically calculate flight routes based on terrain data, reducing the workload of previous manual non-horizontal route design.

以上所述仅为本发明的实施例而已,并不用于限制本发明,对于本领域的技术人员来说,本发明可以有各种更改和变化。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的权利要求范围之内。The above description is only an embodiment of the present invention, and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and changes. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the scope of the claims of the present invention.

Claims (9)

1.一种基于地形高程的非水平航线设计方法,其特征在于,包括:1. a non-horizontal route design method based on terrain elevation, is characterized in that, comprises: 确定待测区域内的起算航线,基于预设的采样间距在所述起算航线上采集若干个采样点;Determine the starting route in the area to be measured, and collect several sampling points on the starting route based on the preset sampling interval; 将每一个采样点对应的地面点加上预设的相对航高变换为空中点,所有空中点按顺序排列形成空中点集,将所述空中点集通过线性回归进行线段拟合,得到所述起算航线对应的非水平航线,包括:以所述空中点集的起点作为起点将所述空中点集进行线段拟合,当所述空中点集中参与拟合的点到拟合出的线段的高程差值大于预先设定的阈值时,停止拟合,得到第一航段;以所述第一航段作为当前航段,以所述当前航段的终点作为起点继续将剩余的空中点集进行线段拟合,当所述空中点集中参与拟合的点到拟合出的线段的高程差值大于预先设定的阈值时,停止拟合,得到下一航段;以所述下一航段作为当前航段继续进行线段拟合,直到所述空中点集中的空中点全部拟合完毕,得到所述起算航线对应的非水平航线,其中所述非水平航线由多个连续的线段组成;The ground point corresponding to each sampling point plus the preset relative altitude is transformed into an air point, all the air points are arranged in order to form an air point set, and the air point set is subjected to line segment fitting through linear regression to obtain the Calculating the non-horizontal route corresponding to the starting route includes: using the starting point of the aerial point set as the starting point to perform line segment fitting on the aerial point set, and when the aerial point set participates in the fitting point to the height of the fitted line segment When the difference is greater than the preset threshold, stop fitting to obtain the first segment; take the first segment as the current segment, and continue to carry out the remaining aerial point sets with the end point of the current segment as the starting point. Line segment fitting, when the height difference between the points participating in the fitting in the air point set and the fitted line segment is greater than a preset threshold, stop the fitting, and obtain the next flight segment; Continue to perform line segment fitting as the current flight segment until all the air points in the air point set are fitted, and obtain a non-horizontal route corresponding to the starting route, wherein the non-horizontal route is composed of a plurality of continuous line segments; 以所述起算航线作为参考航线,根据预设的旁向间距得到邻近航线,将所述邻近航线对应的空中点集通过线性回归进行线段拟合得到所述邻近航线对应的非水平航线;Taking the starting route as a reference route, obtaining an adjacent route according to a preset lateral spacing, and performing line segment fitting on the air point set corresponding to the adjacent route through linear regression to obtain a non-horizontal route corresponding to the adjacent route; 计算参考航线对应的非水平航线与所述邻近航线对应的非水平航线的重叠度,当所述重叠度满足预设的条件时,所述邻近航线对应的非水平航线即为所述待测区域内的下一条非水平航线;Calculate the degree of overlap between the non-horizontal air route corresponding to the reference air route and the non-horizontal air route corresponding to the adjacent air route. When the overlap degree satisfies a preset condition, the non-horizontal air route corresponding to the adjacent air route is the area to be measured the next non-horizontal route within the 以所述计算出的邻近航线作为新的参考航线,继续敷设非水平航线,直到敷设的当前非水平航线的旁向方向坐标值不位于所述待测区域旁向方向的最大坐标值和最小坐标值之间时,停止航敷设。Taking the calculated adjacent route as a new reference route, continue to lay the non-horizontal route until the lateral direction coordinate value of the current non-horizontal route being laid is not located in the maximum coordinate value and the minimum coordinate of the lateral direction of the area to be measured When the value is between, stop the air laying. 2.如权利要求1所述的基于地形高程的非水平航线设计方法,其特征在于,确定待测区域内的起算航线,包括:2. the non-horizontal route design method based on terrain elevation as claimed in claim 1 is characterized in that, determining the starting route in the area to be measured, comprising: 基于航线设计方向,将起算航线的Y值设置为(Ymin+Ymax)/2,获取所述起算航线与所述待测区域的交点,以确定所述起算航线的起点坐标和终点坐标;其中Ymin为所述待测区域角点的最小Y值坐标,Ymax为所述待测区域角点的最大Y值坐标。Based on the route design direction, the Y value of the starting route is set to (Y min +Y max )/2, and the intersection point of the starting route and the area to be measured is obtained to determine the start and end coordinates of the starting route; Wherein Y min is the minimum Y value coordinate of the corner point of the area to be measured, and Y max is the maximum Y value coordinate of the corner point of the area to be measured. 3.如权利要求1所述的基于地形高程的非水平航线设计方法,其特征在于,以所述起算航线作为参考航线,根据预设的旁向间距得到邻近航线,包括:3. the non-horizontal route design method based on terrain elevation as claimed in claim 1, is characterized in that, with described starting route as reference route, obtain adjacent route according to preset side spacing, comprising: 以所述起算航线作为参考航线,利用所述参考航线的Y坐标加上或减去预设的旁向间距,得到邻近航线的Y坐标;Taking the starting route as the reference route, and using the Y coordinate of the reference route to add or subtract the preset side spacing, the Y coordinate of the adjacent route is obtained; 基于航线设计方向和所述邻近航线的Y坐标,获取所述邻近航线与所述待测区域的交点,以确定所述邻近航线的起点坐标和终点坐标,得到邻近航线。Based on the route design direction and the Y coordinate of the adjacent route, the intersection of the adjacent route and the area to be measured is obtained to determine the start and end coordinates of the adjacent route to obtain the adjacent route. 4.如权利要求1所述的基于地形高程的非水平航线设计方法,其特征在于,计算参考航线对应的非水平航线与所述邻近航线对应的非水平航线的重叠度,当所述重叠度满足预设的条件时,所述邻近航线对应的非水平航线即为所述待测区域内的下一条非水平航线,包括:4. the non-horizontal route design method based on terrain elevation as claimed in claim 1 is characterized in that, calculating the overlap degree of the non-horizontal route corresponding to the reference route and the non-horizontal route corresponding to the adjacent route, when the overlap degree When the preset conditions are met, the non-horizontal route corresponding to the adjacent route is the next non-horizontal route in the area to be measured, including: 利用共线方程数学模型计算所述邻近航线对应的非水平航线的地面覆盖范围;Calculate the ground coverage of the non-horizontal air route corresponding to the adjacent air route by using a collinear equation mathematical model; 利用共线方程数学模型计算所述参考航线对应的非水平航线的地面覆盖范围;Calculate the ground coverage of the non-horizontal route corresponding to the reference route by using a collinear equation mathematical model; 获取上述两个地面覆盖范围的交集多边形在Y方向的最窄距离,所述最窄距离除以基准面旁向幅宽得到最小重叠度;Obtain the narrowest distance in the Y direction of the intersection polygon of the above-mentioned two ground coverage areas, and divide the narrowest distance by the lateral width of the reference plane to obtain the minimum overlap; 计算所述最小重叠度与预设的设计重叠度的差值,当所述差值满足预设的阈值时,所述邻近航线对应的非水平航线即为即为所述待测区域内的下一条非水平航线。Calculate the difference between the minimum overlap degree and the preset design overlap degree. When the difference satisfies the preset threshold, the non-horizontal air route corresponding to the adjacent air route is the lower air route in the area to be measured. A non-horizontal route. 5.如权利要求1所述的基于地形高程的非水平航线设计方法,其特征在于,还包括:5. the non-horizontal route design method based on terrain elevation as claimed in claim 1, is characterized in that, also comprises: 当所述重叠度不满足预设的条件时,计算所述邻近航线Y坐标的调整量;When the overlapping degree does not meet the preset condition, calculate the adjustment amount of the Y coordinate of the adjacent air route; 根据所述邻近航线Y坐标的调整量调整所述邻近航线的Y坐标,并重新求得调整后的邻近航向的起点坐标和终点坐标,及进行非水平航线拟合和重叠度计算,直到当重新计算的重叠度满足预设的条件。Adjust the Y coordinate of the adjacent route according to the adjustment amount of the Y coordinate of the adjacent route, and re-obtain the adjusted start and end coordinates of the adjacent route, and perform non-horizontal route fitting and overlap calculation until the new The calculated overlap degree satisfies the preset condition. 6.如权利要求1~5任一项所述的基于地形高程的非水平航线设计方法,其特征在于,在确定起算航线的位置之前,还包括:6. The method for designing a non-horizontal route based on terrain elevation according to any one of claims 1 to 5, wherein before determining the position of the starting route, the method further comprises: 根据航线敷设方向进行坐标系旋转,以使得旋转后坐标系的X轴平行于敷设的航线;Rotate the coordinate system according to the route laying direction, so that the X axis of the coordinate system after the rotation is parallel to the route laid; 确定航线方向为坐标系的X轴,以及确定航线的旁向方向为坐标系的Y轴。Determine the route direction as the X axis of the coordinate system, and determine the side direction of the route as the Y axis of the coordinate system. 7.如权利要求1~5任一项所述的基于地形高程的非水平航线设计方法,其特征在于,在停止航线敷设之后,还包括:7. The non-horizontal route design method based on terrain elevation according to any one of claims 1 to 5, characterized in that, after stopping the route laying, further comprising: 进行坐标系反变换,重新确定新的航线坐标,以将航线坐标变换为地图投影坐标系下的坐标。Perform the inverse transformation of the coordinate system, and re-determine the new route coordinates, so as to transform the route coordinates into the coordinates in the map projection coordinate system. 8.一种终端,其特征在于,所述终端包括:存储器、处理器及存储在所述存储器上并可在所述处理器上运行的计算机程序,所述计算机程序被所述处理器执行时实现如权利要求1~5中任一项所述的基于地形高程的非水平航线设计方法的步骤。8. A terminal, characterized in that the terminal comprises: a memory, a processor, and a computer program stored on the memory and executable on the processor, when the computer program is executed by the processor The steps of implementing the method for designing a non-horizontal route based on terrain elevation as claimed in any one of claims 1 to 5. 9.一种存储介质,其特征在于,所述存储介质上存储有基于地形高程的非水平航线设计程序,所述基于地形高程的非水平航线设计程序被处理器执行时实现如权利要求1~5中任一项所述的基于地形高程的非水平航线设计方法的步骤。9. A storage medium, characterized in that, a non-horizontal route design program based on terrain elevation is stored on the storage medium, and the non-horizontal route design program based on terrain elevation is implemented by a processor as claimed in claim 1 to Steps of the method for designing a non-horizontal route based on terrain elevation described in any one of 5.
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