[go: up one dir, main page]

CN111508327A - A target system in which the earth's north and south poles rapidly rotate around the geocentric axis - Google Patents

A target system in which the earth's north and south poles rapidly rotate around the geocentric axis Download PDF

Info

Publication number
CN111508327A
CN111508327A CN202010342743.2A CN202010342743A CN111508327A CN 111508327 A CN111508327 A CN 111508327A CN 202010342743 A CN202010342743 A CN 202010342743A CN 111508327 A CN111508327 A CN 111508327A
Authority
CN
China
Prior art keywords
polar
earth
simulation unit
imaging
north
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN202010342743.2A
Other languages
Chinese (zh)
Inventor
杨秀彬
韩金良
王绍恩
岳炜
徐婷婷
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Changchun Institute of Optics Fine Mechanics and Physics of CAS
Original Assignee
Changchun Institute of Optics Fine Mechanics and Physics of CAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Changchun Institute of Optics Fine Mechanics and Physics of CAS filed Critical Changchun Institute of Optics Fine Mechanics and Physics of CAS
Priority to CN202010342743.2A priority Critical patent/CN111508327A/en
Publication of CN111508327A publication Critical patent/CN111508327A/en
Pending legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B25/00Models for purposes not provided for in G09B23/00, e.g. full-sized devices for demonstration purposes

Landscapes

  • Engineering & Computer Science (AREA)
  • Business, Economics & Management (AREA)
  • Physics & Mathematics (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Studio Devices (AREA)

Abstract

一种地球南北极地景物绕地心轴线快速旋转的靶标系统属于空间光学遥感技术领域,解决了地球南北极区域绕地轴快速转动、引起地表切向速度变化快、方向各异、大小不均衡等问题。该系统包括:极地模拟单元,成像模拟单元和驱动控制单元;极地模拟单元按照比例模拟纬度60°以上自转的地球,并模拟地球的俯视图;成像模拟单元模拟卫星位于极地模拟单元上空运动和对极地模拟单元成像;驱动控制单元驱动极地模拟单元旋转,并控制成像模拟单元的成像速度。本发明模拟真实情况下卫星对南北极地景物的成像情况;不仅可以对极地景物的拍摄效果进行仿真,还同时具备对极地不同区域形成的像移速度进行定标的能力,通过具体计算即可得到像移合速度的大小和方向。

Figure 202010342743

A target system in which the north and south poles of the earth rapidly rotate around the geocentric axis belongs to the field of space optical remote sensing technology, and solves the problems of rapid rotation around the earth's axis in the north and south poles of the earth, causing rapid changes in the surface tangential speed, different directions, and unbalanced sizes. . The system includes: a polar simulation unit, an imaging simulation unit and a drive control unit; the polar simulation unit simulates the earth rotating at a latitude above 60° according to the scale, and simulates the top view of the earth; the imaging simulation unit simulates the movement of the satellite over the polar simulation unit and the anti-polarity The simulation unit is imaging; the driving control unit drives the polar simulation unit to rotate, and controls the imaging speed of the imaging simulation unit. The invention simulates the imaging situation of the North and South Pole landscapes by satellites under real conditions; it can not only simulate the shooting effect of the polar landscapes, but also has the ability to calibrate the image movement speeds formed in different regions of the polar regions, which can be obtained through specific calculations. Like the magnitude and direction of the transition velocity.

Figure 202010342743

Description

一种地球南北极地景物绕地心轴线快速旋转的靶标系统A target system in which the earth's north and south poles rapidly rotate around the geocentric axis

技术领域technical field

本发明属于空间光学遥感技术领域,具体涉及一种地球南北极地景物绕地心轴线快速旋转的靶标系统。The invention belongs to the technical field of space optical remote sensing, and in particular relates to a target system in which the earth's north and south poles rapidly rotate around the earth's central axis.

背景技术Background technique

地球的南北两极是地球生态环境重要的组成部分,也是全球气候变化的温度计,因此各国对于极地的科研考察从未停下脚步。近年来,由于人类不合自然规律的活动,全球气候变暖问题不断加剧,极地冰川融化速度加快,海平面上升,生态遭到严重破坏,由此引发的灾害频频发生。极地的生态环境急需全人类关注,但是南北两极由于其极寒的温度人烟稀少,对其环境的监测难度十分巨大,由此易见空间光学遥感技术成为最好手段,航天领域在极地科考的作用愈发重要。但是天基技术存在着成本高、风险大等特点,发射前的地面实验、仿真对其应用起着至关重要的作用,这就要求仿真系统具有高保真度,实验结果具有真实、有效、可靠等特点,从而降低科研风险。The north and south poles of the earth are an important part of the earth's ecological environment, and they are also the thermometers of global climate change. Therefore, the scientific research and investigation of the polar regions has never stopped. In recent years, due to the unnatural activities of human beings, the problem of global warming has been intensified, the melting speed of polar glaciers has accelerated, the sea level has risen, and the ecology has been severely damaged, resulting in frequent disasters. The ecological environment of the polar regions urgently needs the attention of all human beings. However, due to its extremely cold temperature and sparse population, it is very difficult to monitor its environment. It is easy to see that space optical remote sensing technology has become the best means. The role of aerospace in polar scientific research increasingly important. However, space-based technology has the characteristics of high cost and high risk. The ground experiment and simulation before launch play a crucial role in its application, which requires the simulation system to have high fidelity and the experimental results to be real, effective and reliable. and other characteristics, thereby reducing the risk of scientific research.

由于地球自转等因素影响,传统卫星成像通常集中在南北纬65°或70° 以内的区域,成像方式多为星下点成像或侧摆成像,像移速度为卫星飞行速 度在地球上的投影和地球自转切向速度的二维合速度,在低纬度区变化较为 缓慢,易于测量修正,如图1所示,然而随着纬度增加,极地区域地面转动 速度相对于卫星运动变化愈发复杂,极点周围的速度方向大小更是各处不同。 由于这种运动的复杂性,此过程产生的像移对成像影响非常严重,常规的模 拟装置无法满足此种复杂的模拟要求,且国内外对于这种非常规的运动模拟尚缺乏有效手段,需要一种对地球南北极地成像的地面演示系统,为极地成 像质量的分析提供有力指导,因此提出一种地球南北极地景物绕地心轴线快 速旋转的靶标系统。Due to factors such as the earth's rotation, traditional satellite imaging is usually concentrated in areas within 65° or 70° north-south latitude, and the imaging methods are mostly sub-satellite point imaging or side-swing imaging. The two-dimensional combined velocity of the tangential velocity of the Earth's rotation changes slowly in low latitudes and is easy to measure and correct, as shown in Figure 1. However, as the latitude increases, the ground rotation velocity in the polar regions changes more and more complicated relative to the satellite motion. The size of the surrounding speed direction is different everywhere. Due to the complexity of this motion, the image shift produced by this process has a very serious impact on imaging. Conventional simulation devices cannot meet such complex simulation requirements, and there is still no effective means for such unconventional motion simulation at home and abroad. A ground demonstration system for imaging the north and south poles of the earth provides powerful guidance for the analysis of polar imaging quality. Therefore, a target system for rapidly rotating the earth's north and south poles around the geocentric axis is proposed.

发明内容SUMMARY OF THE INVENTION

为了解决现有技术中存在的问题,本发明提供了一种地球南北极地景物绕地心轴线快速旋转的靶标系统,解决了地球南北极区域绕地轴快速转动、引起地表切向速度变化快、方向各异、大小不均衡等问题。In order to solve the problems existing in the prior art, the present invention provides a target system in which the north and south poles of the earth rapidly rotate around the earth's central axis, which solves the problem of the rapid rotation of the earth's north and south poles around the earth's axis, causing rapid changes in the surface tangential speed and direction. Different, uneven size, etc.

本发明解决技术问题所采用的技术方案如下:The technical scheme adopted by the present invention to solve the technical problem is as follows:

一种地球南北极地景物绕地心轴线快速旋转的靶标系统,该系统包括:极地模拟单元,成像模拟单元和驱动控制单元;A target system that rapidly rotates around the center axis of the earth's north and south poles, the system comprises: a polar simulation unit, an imaging simulation unit and a drive control unit;

所述极地模拟单元按照比例模拟纬度60°以上自转的地球,并模拟地球的俯视图;The polar simulation unit simulates the earth rotating above 60° latitude according to the scale, and simulates the top view of the earth;

所述成像模拟单元模拟卫星位于所述极地区域上空运动和对所述极地模拟单元成像;The imaging simulation unit simulates the movement of a satellite over the polar region and images the polar simulation unit;

所述驱动控制单元驱动所述极地模拟单元旋转,并控制所述成像模拟单元的成像速度。The driving control unit drives the polar simulation unit to rotate, and controls the imaging speed of the imaging simulation unit.

优选的,所述极地模拟单元包括水平转动平台,设置在所述水平转动平台上的极地模型,和设置在所述极地模型上的极地靶标;Preferably, the polar simulation unit includes a horizontal rotating platform, a polar model arranged on the horizontal rotating platform, and a polar target arranged on the polar model;

所述成像模拟单元包括:安装在所述极地模型上方的相机运动轨道,设置在所述相机运动轨道上的相机架,和安装在所述相机架上的工业相机;The imaging simulation unit includes: a camera motion track installed above the polar model, a camera frame arranged on the camera motion track, and an industrial camera installed on the camera frame;

所述驱动控制单元包括:与所述水平转动平台和所述相机架连接的驱动装置,和安装在所述驱动装置上,控制所述水平转动平台和所述相机架转速的驱动控制装置。The drive control unit includes: a drive device connected to the horizontal rotation platform and the camera frame, and a drive control device mounted on the drive device to control the rotational speeds of the horizontal rotation platform and the camera frame.

优选的,所述极地模型和所述极地靶标按照1:1000000比例模拟地球。Preferably, the polar model and the polar target simulate the earth at a scale of 1:1000000.

优选的,所述极地靶标的内容可更换。Preferably, the content of the polar target is replaceable.

优选的,所述相机运动轨道与所述极地模型的弧度相同。Preferably, the motion trajectory of the camera is the same as the arc of the polar model.

本发明的有益效果是:本发明根据缩放比例确认极地模型的曲率半径大小、转动平台转速、相机轨道高度、相机运动速度等参数,搭建极地模型及具体成像装置,使极地模型水平转动、相机在轨道上绕模型进行运动拍照,以模拟真实情况下卫星对南北极地景物的成像情况;通过极地模型上的靶标,不仅可以对极地景物的拍摄效果进行仿真,还同时具备对极地不同区域形成的像移速度进行定标的能力,通过具体计算即可得到像移合速度的大小和方向。The beneficial effects of the present invention are as follows: the present invention confirms parameters such as the radius of curvature of the polar model, the rotational speed of the rotating platform, the camera orbit height, and the movement speed of the camera according to the scaling ratio, and builds the polar model and a specific imaging device, so that the polar model is rotated horizontally and the camera is Moving around the model on the orbit to take pictures to simulate the imaging situation of the satellites on the north and south poles in the real situation; through the target on the polar model, not only can the shooting effect of the polar scenery be simulated, but also the image formed in different regions of the polar region can be simulated. The ability to scale the moving speed can be obtained through the specific calculation to obtain the size and direction of the moving speed.

附图说明Description of drawings

图1传统卫星成像演示图。Figure 1 Demonstration of traditional satellite imaging.

图2本发明一种地球南北极地景物绕地心轴线快速旋转的靶标系统北极地区像移速度关系示意图。FIG. 2 is a schematic diagram of the relationship between the image movement speed in the Arctic region of a target system in which the earth and the north and south poles of the present invention rapidly rotate around the geocentric axis.

图3本发明一种地球南北极地景物绕地心轴线快速旋转的靶标系统模拟装置侧视图。Fig. 3 is a side view of a target system simulation device in which the earth's north and south poles rapidly rotate around the earth's central axis according to the present invention.

图4本发明一种地球南北极地景物绕地心轴线快速旋转的靶标系统模拟装置俯视图。FIG. 4 is a top view of a target system simulation device of the present invention in which the earth's north and south poles rapidly rotate around the geocentric axis.

图中:1、水平转动平台,2、极地模型,3、极地靶标,4、工业相机,5、固定装置,6、相机运动轨道,7、驱动装置。In the picture: 1. Horizontal rotation platform, 2. Polar model, 3. Polar target, 4. Industrial camera, 5. Fixing device, 6. Camera motion track, 7. Driving device.

具体实施方式Detailed ways

下面结合附图和实施例对本发明做进一步详细说明。The present invention will be described in further detail below with reference to the accompanying drawings and embodiments.

如图2和图3所示,一种地球南北极地景物绕地心轴线快速旋转的靶标系统,该系统包括:极地模拟单元,成像模拟单元,驱动控制单元;As shown in Figures 2 and 3, a target system for rapidly rotating the earth's north and south poles around the geocentric axis, the system includes: a polar simulation unit, an imaging simulation unit, and a drive control unit;

极地模拟单元包括水平转动平台1,极地模型2和极地靶标3;The polar simulation unit includes a horizontal rotation platform 1, a polar model 2 and a polar target 3;

成像模拟单元包括工业相机4,相机架和相机运动轨道6;The imaging simulation unit includes an industrial camera 4, a camera frame and a camera motion track 6;

驱动控制单元包括驱动装置7和驱动控制装置。The drive control unit includes a drive device 7 and a drive control device.

极地模型2默认以1:1000000的比例模拟纬度60°以上的地球。具体做法将地球视为球体,两极地位于正上和正下方,将该比例的地球模型在60°纬度处以垂直地轴的水平面切开球体并取其上半部分,得到底面半径为 3.2m、高约0.8m、弧面曲率半径6.4m的球冠。其中纬度66.5°为极圈所在处,同时极地模型2上装有用于验证和测量的极地靶标3。Polar Model 2 simulates the Earth above 60° latitude at a scale of 1:1000000 by default. The specific method takes the earth as a sphere, and the poles are located directly above and below. The scale of the earth model is cut at 60° latitude with the horizontal plane of the vertical axis and the upper half is taken. The radius of the bottom surface is 3.2m and the height is about 0.8m spherical cap with camber radius of 6.4m. The latitude 66.5° is where the polar circle is located, and the polar model 2 is equipped with a polar target 3 for verification and measurement.

极地靶标3设置在所述极地模型2表面,根据实验内容可进行更换,默认为1:1000000比例的地球俯视图,表面积约为34.5平方米。可以通过相机拍摄极地靶标在地球自转和卫星运动情况下的照片,准确模拟卫星位于极地上空对地面的成像情况,可对极地不同区域形成的像移速度进行定标。The polar target 3 is set on the surface of the polar model 2, and can be replaced according to the experimental content. The default is a 1:1000000 scale top view of the earth, and the surface area is about 34.5 square meters. The camera can take pictures of the polar target under the condition of the earth's rotation and satellite motion, accurately simulate the imaging situation of the satellite on the ground in the polar sky, and can calibrate the image movement speed formed in different regions of the polar region.

所述极地模型2设置在水平转动平台1上,用于带动极地模型2进行转动,所述极地模型2上配有用于固定极地模型2的装置,下方由驱动转置7 提供转动力矩,带动所述水平转动平台1进行水平周期转动,模拟地球极地绕地轴的自转,自转周期默认地球自转周期,自转的平均角速度 0.00007292rad/s。The polar model 2 is arranged on the horizontal rotating platform 1, and is used to drive the polar model 2 to rotate. The polar model 2 is equipped with a device for fixing the polar model 2, and the lower part is provided by the driving transposition 7. The horizontal rotation platform 1 performs horizontal periodic rotation to simulate the rotation of the earth's pole around the earth's axis.

成像模拟单元中相机运动轨道6通过固定结构5设置在所述极地模型2 的上方,为与极地模型2比例相同的圆弧形导轨,弧度与极地模型2上表面相同,相机运动轨道6距模型高度为0.5m,曲率半径6.9m。通过相机架将工业相机4固定于相机运动轨道6上,通过驱动装置带动工业相机4在相机运动轨道6上进行运动,默认速度为0.0076m/s。In the imaging simulation unit, the camera movement track 6 is set above the polar model 2 through the fixed structure 5, which is an arc-shaped guide rail with the same scale as the polar model 2, and the radian is the same as the upper surface of the polar model 2. The camera movement track is 6 distances from the model. The height is 0.5m, and the radius of curvature is 6.9m. The industrial camera 4 is fixed on the camera motion track 6 by the camera frame, and the industrial camera 4 is driven to move on the camera motion track 6 by the driving device, and the default speed is 0.0076m/s.

驱动单元连接着水平转动平台1和相机架,通过对驱动控制装置的设置,所述驱动装置7控制水平转动平台1转速,使其保持水平匀速转动,模拟地球自转在极地地区的运动情况,南北极转动方向不同;通过设置驱动控制装置,所述驱动装置7控制工业相机4在相机运动轨道6上进行匀速运动,模拟卫星位于极地上空的运动情况。The drive unit is connected to the horizontal rotating platform 1 and the camera frame. Through the setting of the drive control device, the drive device 7 controls the rotational speed of the horizontal rotating platform 1 to keep it rotating at a constant horizontal speed, simulating the movement of the earth's rotation in the polar regions, north and south. The poles rotate in different directions; by setting the drive control device, the drive device 7 controls the industrial camera 4 to move at a uniform speed on the camera movement track 6, simulating the movement of the satellite over the pole.

使用前首先根据模拟的缩放比例计算极地模型2的曲率半径大小、水平转动平台1及驱动轮转速、相机运动轨道6距离极地模型2表面距离及其位置、工业相机4运动速度,调试模拟用的工业相机4。Before use, first calculate the radius of curvature of the polar model 2, the rotational speed of the horizontal rotation platform 1 and the driving wheel, the distance between the camera motion track 6 and the surface of the polar model 2 and its position, and the motion speed of the industrial camera 4, which are used for debugging and simulation. Industrial Camera 4.

确认所有装置的控制情况后安装极地模拟单元,依据模拟立体成像的缩放比例选择极地模型2,搭建模型所需曲率半径的圆弧面支撑框架并将其安装于水平转动平台1上,安装驱动轮、传动带等控制转动平台转动的驱动装置7。安装成像模拟单元,将圆弧导轨两端通过固定装置5固定在所需相机运动轨道6处,安装工业相机,使其能够对极地模型2成像。输入控制参数,启动驱动控制装置,控制极地模型2转动和工业相机4运动,进行成像模拟。After confirming the control of all the devices, install the polar simulation unit, select the polar model 2 according to the scaling ratio of the simulated stereo imaging, build the arc surface support frame with the required curvature radius of the model and install it on the horizontal rotation platform 1, install the driving wheel , transmission belt, etc. to control the driving device 7 for the rotation of the rotating platform. Install the imaging simulation unit, fix both ends of the arc guide rail at the required camera motion track 6 through the fixing device 5, and install the industrial camera so that it can image the polar model 2. Input control parameters, start the drive control device, control the rotation of the polar model 2 and the movement of the industrial camera 4, and perform imaging simulation.

以北极地区为例,卫星以推扫方式成像,轨道倾角97°,成像区域如图 2所示,地球自转周期T=23h56min=86160s,自转的平均角速度为Taking the Arctic region as an example, the satellite is imaged in a push-broom manner, with an orbital inclination of 97°. The imaging area is shown in Figure 2. The Earth's rotation period is T=23h56min=86160s, and the average angular velocity of the rotation is

Figure BDA0002469066520000041
Figure BDA0002469066520000041

以此得出转动平台的转动周期及角速度。取地球半径R=6400km,根据原理可知在计算时可先计算实际速度,再通过比例进行换算。则不同纬度处的地球自转线速度为From this, the rotation period and angular velocity of the rotating platform are obtained. Taking the earth's radius R=6400km, according to the principle, it can be known that the actual speed can be calculated first, and then converted by the ratio. Then the linear velocity of the Earth's rotation at different latitudes is

Figure BDA0002469066520000051
Figure BDA0002469066520000051

通过计算可以得出60°纬度上的地球自转线速度The linear velocity of the earth's rotation at 60° latitude can be obtained by calculation

Figure BDA0002469066520000052
Figure BDA0002469066520000052

同理极圈的自转线速度v2=186m/s,75°纬度上线速度v3=121m/s。Similarly, the rotational speed of the polar circle is v 2 =186m/s, and the linear speed of 75° latitude is v 3 =121m/s.

轨道高度H为500km的卫星运行速度The speed of the satellite at an orbital altitude H of 500km

Figure BDA0002469066520000053
Figure BDA0002469066520000053

则其地面上的投影速度then its projected velocity on the ground

Figure BDA0002469066520000054
Figure BDA0002469066520000054

根据1∶1000000比例可以得出对应极地模型2上的各点像移的真实线速度,具体为According to the ratio of 1:1000000, the real linear velocity of the image movement corresponding to each point on the polar model 2 can be obtained, which is specifically:

Figure BDA0002469066520000055
Figure BDA0002469066520000055

v2=0.000186m/s,v 2 =0.000186m/s,

v3=0.00012lm/s,v 3 =0.00012lm/s,

v0=0.00762m/s,v 0 =0.00762m/s,

vs=0.007067m/sv s = 0.007067m/s

其中v0即为工业相机4在相机运动轨道6上的运行线速度。根据比例得出极地模型曲率半径大小为Rp=640000/1000000=6.4m,500km轨道高度的卫星模拟导轨距球面高度Hs=0.5m,曲率半径6.9m。根据相机运动轨道6倾角安装极地模型2,通过固定装,5固定相机运动轨道6两端,将极地模型2自转角速度和工业相机4运行速度输入至驱动控制装置,使系统开始工作。Wherein v 0 is the running linear velocity of the industrial camera 4 on the camera motion track 6 . According to the scale, the radius of curvature of the polar model is R p =640000/1000000 = 6.4m, and the distance between the 500km orbital height of the satellite simulation guide rail and the spherical height H s =0.5m, and the radius of curvature is 6.9m. Install the polar model 2 according to the inclination of the camera motion track 6, fix both ends of the camera motion track 6 through the fixing device 5, and input the rotation angular velocity of the polar model 2 and the running speed of the industrial camera 4 to the drive control device, so that the system starts to work.

如图4所示,以A点为例,虚线表示的像移合速度,地球自转线速度v和投影速度vs之间的夹角ρ,其大小及方向如下As shown in Figure 4, taking point A as an example, the image shift speed represented by the dotted line, the angle ρ between the earth's rotation linear speed v and the projection speed v s , its size and direction are as follows

Figure BDA0002469066520000061
Figure BDA0002469066520000061

地球自转线速度v和投影速度vs的合速度为:The combined velocity of the Earth's rotational linear velocity v and the projected velocity v s is:

Figure BDA0002469066520000062
Figure BDA0002469066520000062

所述合速度与卫星运行速度方向的偏角为:The declination angle between the resultant velocity and the direction of the satellite running velocity is:

Figure BDA0002469066520000063
Figure BDA0002469066520000063

则模型上A点合速度vA=0.007126m/s,方向偏右γA=1.4239°Then the resultant velocity v A = 0.007126m/s at point A on the model, and the direction is to the right γ A = 1.4239°

B点合速度vB=0.007124m/s,方向偏右γB=0.8584°B point speed v B =0.007124m/s, direction to the right γ B =0.8584°

C点合速度vC=0.007124m/s,方向偏左γC=0.8584°C point speed v C = 0.007124m/s, direction left γ C = 0.8584°

D点合速度vD=0.007126m/s,方向偏左γD=1.4239°。D point speed v D =0.007126m/s, the direction is left γ D =1.4239°.

Claims (5)

1. A target system for rapid rotation of a north-south earth scene about a geocentric axis, the system comprising: a polar region simulation unit, an imaging simulation unit and a drive control unit;
the polar region simulation unit simulates the earth rotating at a latitude of more than 60 degrees in proportion and simulates a top view of the earth;
the imaging simulation unit simulates the satellite to move over the polar region and images the polar simulation unit;
the driving control unit drives the polar region simulation unit to rotate and controls the imaging speed of the imaging simulation unit.
2. The target system of claim 1, wherein the target system for fast rotation of the Earth's north-south polar scene about the Earth's center axis,
the polar region simulation unit comprises a horizontal rotating platform, a polar region model arranged on the horizontal rotating platform and a polar region target arranged on the polar region model;
the imaging simulation unit includes: a camera motion track mounted above the polar model, a camera frame disposed on the camera motion track, and an industrial camera mounted on the camera frame;
the drive control unit includes: the camera comprises a driving device connected with the horizontal rotating platform and the camera frame, and a driving control device arranged on the driving device and used for controlling the rotating speed of the horizontal rotating platform and the camera frame.
3. The target system of claim 2, wherein the polar model and the polar target simulate the earth on a 1:1000000 scale.
4. The target system of claim 2, wherein the contents of the polar target are replaceable.
5. The target system of claim 2, wherein the camera motion trajectory is the same arc as the polar model.
CN202010342743.2A 2020-04-27 2020-04-27 A target system in which the earth's north and south poles rapidly rotate around the geocentric axis Pending CN111508327A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202010342743.2A CN111508327A (en) 2020-04-27 2020-04-27 A target system in which the earth's north and south poles rapidly rotate around the geocentric axis

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202010342743.2A CN111508327A (en) 2020-04-27 2020-04-27 A target system in which the earth's north and south poles rapidly rotate around the geocentric axis

Publications (1)

Publication Number Publication Date
CN111508327A true CN111508327A (en) 2020-08-07

Family

ID=71874719

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202010342743.2A Pending CN111508327A (en) 2020-04-27 2020-04-27 A target system in which the earth's north and south poles rapidly rotate around the geocentric axis

Country Status (1)

Country Link
CN (1) CN111508327A (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6353474B1 (en) * 2000-04-13 2002-03-05 Hughes Electronics Corporation High accuracy data acquisition port for environmental chamber photogrammetry
CN201035826Y (en) * 2007-05-08 2008-03-12 张改一 Solar system simulation demonstrator
CN204463691U (en) * 2015-03-10 2015-07-08 中国科学技术馆 Dynamic Demonstration Installation for Geostationary and Polar Orbiting Satellite Operational Services
CN105931562A (en) * 2016-06-22 2016-09-07 王舒琴 Teaching aid for demonstrating automatic rotation of various artificial satellites and use method of teaching aid
CN108257500A (en) * 2018-04-16 2018-07-06 浙江环艺电子科技有限公司 For the illuminated model of touch of geographical teaching
CN108710379A (en) * 2018-06-14 2018-10-26 上海卫星工程研究所 Fixed statellite is imaged Yaw steering angle computational methods
CN109640076A (en) * 2018-12-31 2019-04-16 中国科学院长春光学精密机械与物理研究所 A kind of ground semi-physical simulation platform of the vertical rail Overlap-scanning imaging of space camera
CN110986886A (en) * 2019-12-18 2020-04-10 中国科学院长春光学精密机械与物理研究所 Double-camera dynamic rotation scanning three-dimensional imaging simulation device

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6353474B1 (en) * 2000-04-13 2002-03-05 Hughes Electronics Corporation High accuracy data acquisition port for environmental chamber photogrammetry
CN201035826Y (en) * 2007-05-08 2008-03-12 张改一 Solar system simulation demonstrator
CN204463691U (en) * 2015-03-10 2015-07-08 中国科学技术馆 Dynamic Demonstration Installation for Geostationary and Polar Orbiting Satellite Operational Services
CN105931562A (en) * 2016-06-22 2016-09-07 王舒琴 Teaching aid for demonstrating automatic rotation of various artificial satellites and use method of teaching aid
CN108257500A (en) * 2018-04-16 2018-07-06 浙江环艺电子科技有限公司 For the illuminated model of touch of geographical teaching
CN108710379A (en) * 2018-06-14 2018-10-26 上海卫星工程研究所 Fixed statellite is imaged Yaw steering angle computational methods
CN109640076A (en) * 2018-12-31 2019-04-16 中国科学院长春光学精密机械与物理研究所 A kind of ground semi-physical simulation platform of the vertical rail Overlap-scanning imaging of space camera
CN110986886A (en) * 2019-12-18 2020-04-10 中国科学院长春光学精密机械与物理研究所 Double-camera dynamic rotation scanning three-dimensional imaging simulation device

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
中国航天日: ""风云"气象知多少", 《HTTPS://TECH.SINA.COM.CN/D/S/2020-04-15/DOC-IIRCZYMI6456493.SHTML》 *

Similar Documents

Publication Publication Date Title
CN106124170B (en) A kind of camera optical axis direction computational methods based on high-precision attitude information
JP6228679B2 (en) Gimbal and gimbal simulation system
CN107152926B (en) A kind of satellite quickly rotates super large breadth sweeping imaging method
CN103886208B (en) High-resolution optical satellite maneuvering imaging drift angle correction method
US10167093B2 (en) Apparatus and method for controlling a satellite
CN110986886A (en) Double-camera dynamic rotation scanning three-dimensional imaging simulation device
CN111079291B (en) Moonlet splicing imaging ground simulation system
CN105136164B (en) Consider the comprehensive staring imaging emulation moved of satellite and method for evaluating quality and device
CN106054910B (en) The adjustable satellite in visual field direction stares attitude control method over the ground
CN106197434A (en) The computational methods at attitude of satellite angle based on ground target point position
CN112009708B (en) Fixed-wing unmanned aerial vehicle, single-lens oblique photography system and method
CN105444781A (en) Ground verification method for satellite-borne autonomously guided imaging
CN107525492A (en) A kind of drift angle simulating analysis suitable for quick earth observation satellite
CN104144304B (en) A kind of high resolution camera difference visual field time of integration determines method
CN113781885B (en) A simulation device for three-degree-of-freedom dynamic two-dimensional annular scan space imaging
CN109828362B (en) Ultra-large-width imaging method based on whole-satellite fast swing
CN105005310B (en) A kind of attitude adjusting method being imaged along slanted bar band
US1586070A (en) Method of taking photographs and camera mounting for use in connection therewith
CN106908085B (en) A kind of starlight measurement direction control method based on earth rotation compensation
CN111508327A (en) A target system in which the earth's north and south poles rapidly rotate around the geocentric axis
KR101885920B1 (en) An astronomical device and its driving method for calculating astronomical physical quantity and tracking sun position with automatic tracking function
CN111121765A (en) Method for skillfully observing earth and monitoring GEO target by using common remote sensing satellite platform
JPS58115388A (en) Sunshine simulator
US1559688A (en) Apparatus for photographic cartography
CN111127319A (en) A Ground Pixel Resolution Calculation Method for Push-broom Imaging in Motion

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20200807