CN209248859U - A kind of spatial remotely sensed imaging semi-physical simulation platform based on sand table motor pattern - Google Patents
A kind of spatial remotely sensed imaging semi-physical simulation platform based on sand table motor pattern Download PDFInfo
- Publication number
- CN209248859U CN209248859U CN201821075372.0U CN201821075372U CN209248859U CN 209248859 U CN209248859 U CN 209248859U CN 201821075372 U CN201821075372 U CN 201821075372U CN 209248859 U CN209248859 U CN 209248859U
- Authority
- CN
- China
- Prior art keywords
- sand table
- solar simulator
- solar
- camera load
- physical simulation
- 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.)
- Expired - Fee Related
Links
Classifications
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B23/00—Models for scientific, medical, or mathematical purposes, e.g. full-sized devices for demonstration purposes
- G09B23/06—Models for scientific, medical, or mathematical purposes, e.g. full-sized devices for demonstration purposes for physics
-
- G—PHYSICS
- G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
- G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
- G09B23/00—Models for scientific, medical, or mathematical purposes, e.g. full-sized devices for demonstration purposes
- G09B23/06—Models for scientific, medical, or mathematical purposes, e.g. full-sized devices for demonstration purposes for physics
- G09B23/22—Models for scientific, medical, or mathematical purposes, e.g. full-sized devices for demonstration purposes for physics for optics
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Business, Economics & Management (AREA)
- Mathematical Analysis (AREA)
- Mathematical Optimization (AREA)
- Mathematical Physics (AREA)
- Pure & Applied Mathematics (AREA)
- Computational Mathematics (AREA)
- Algebra (AREA)
- Educational Administration (AREA)
- Educational Technology (AREA)
- Theoretical Computer Science (AREA)
- Optics & Photonics (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The utility model proposes a kind of spatial remotely sensed imaging semi-physical simulation platforms based on sand table motor pattern, including kinematic system, camera load, solar simulator system and sand table;Kinematic system includes the gantry being placed on the ground and the track that is slidably connected with gantry;Solar simulator system includes solar simulator and solar light reflecting mirror, solar light reflecting mirror is vertically set on right above solar simulator, solar simulator is placed on the ground, and sand table is placed between track, and the light that solar simulator emits is reflected on sand table by solar light reflecting mirror;The top at gantry is arranged in camera load, as the distance to adjust camera load relative to solar simulator and sand table is moved at gantry in orbit, realizes the imaging to sand table.The utility model is replaced with horizontal imaging in Physical Simulation Platform indoors, solves the problems, such as that physical simulation system deployment space is inadequate, reduce integral construction difficulty by by the relationship that camera load is vertically imaged at substar in remote sensing.
Description
Technical field
The utility model relates to satellite remote sensing technology field more particularly to a kind of space remote sensings based on sand table motor pattern
Semi-physical simulation platform is imaged.
Background technique
Remote sensing refers to non-contacting, remote Detection Techniques.Refer generally to the electromagnetism with sensor/remote sensor to object
The radiation of wave, the detection of reflection characteristic.Remote sensing is by this kind of instrument to sensitive to electromagnetic waves of remote sensor, far from target and non-
Detect Target scalar under contact target object condition, obtain its reflection, radiation or scattering electromagnetic wave information (such as electric field, magnetic field,
The information such as electromagnetic wave, seismic wave), and extract, determine, working process, a science and technology of analysis and application.
Semi-physical simulation is in laboratory conditions, to carry out dynamic simulative emulation, bound fraction meter to each imaging chain
Calculation machine simulation result, it is final to obtain remote sensing emulating image, by surveying close to analog simulation process that is true, can be controlled
The performance of the remote sensing system is tried, and provides evaluation result.
When carrying out imaging experiment using remote sensing satellite, it is easy to be difficult to obtain by the external environment influences such as track and weather
Comprehensive data, it is therefore desirable to experimental data be supplemented by means of emulation experiment.Currently, to remote sensing system into
When row semi-physical simulation, due to the requirement of experiment equipment and experiment effect, biggish place space is generally required.Such as remote sensing system
Solar simulator volume in system is larger, is not suitable for being hung and be moved;The building solar simulator of full dimension, imaging load
Enough activity spaces etc. are needed with the positional relationship of test objective.Therefore carry out design deployment in a smaller space, integrally apply
Work difficulty is larger.
Utility model content
In view of the above problems, the utility model provides one kind and overcomes the above problem or at least be partially solved the above problem
Space base in the spatial remotely sensed imaging semi-physical simulation platform of sand table motor pattern, to solve existing analogue system space for its deployment not
Enough problems, and reduce integral construction difficulty.
It is imitative to provide a kind of spatial remotely sensed imaging semi physical based on sand table motor pattern for the one aspect of the utility model
True platform, including kinematic system, camera load, solar simulator system and sand table;
The kinematic system includes the gantry being placed on the ground and the track that is slidably connected with described gantry;
The solar simulator system includes solar simulator and solar light reflecting mirror, and the solar light reflecting mirror is vertically set
It sets above the solar simulator, the solar simulator is placed on the ground, and the sand table is placed between the track,
The solar light reflecting mirror is used to the light that the solar simulator emits being reflected into the sand table;
The top at described gantry is arranged in the camera load, as described gantry is moved on the track to adjust
Distance of the camera load relative to the solar simulator and the sand table is stated, to realize the imaging to the sand table.
It wherein, further include three axis holders, the camera load is connect by the three axis holder with described gantry, the phase
Airborne lotus is by the way that described gantry is vertical and/or the movement of horizontal movement and the three axis holder pitching and/or rotation, with reality
Now the multi-angle of the sand table is imaged.
It wherein, further include two-dimensional movement turntable, the sand table is arranged between the track two-dimensional movement turntable,
For adjusting the rotation and/or pitching of the sand table.
Wherein, the camera load includes infrared, EO-1 hyperion and low-light camera load, to simulate different remotely sensed image feelings
Condition.
The technical solution provided in the utility model embodiment, at least has the following technical effects or advantages:
For the present embodiment by relationship that the camera load in remote sensing is vertically imaged at substar, physics indoors is imitative
It is replaced in true platform with horizontal imaging, so that solar simulator need not be set up in the sky, thereby reduces difficulty of construction, solved
In the conditional situation of story height, the problem that image-forming range is too short, breadth is too narrow, and then visible light can be supported indoors
Characteristic Simulation, target low-light-level performance simulation study carry out the remotely sensed image experiment and verifying of panchromatic, low-light etc..
The above description is merely an outline of the technical solution of the present invention, in order to better understand the skill of the utility model
Art means, and being implemented in accordance with the contents of the specification, and in order to allow above and other purpose, feature of the utility model
It can be more clearly understood with advantage, it is special below to lift specific embodiment of the present utility model.
Detailed description of the invention
By reading the following detailed description of the preferred embodiment, various other advantages and benefits are common for this field
Technical staff will become clear.The drawings are only for the purpose of illustrating a preferred embodiment, and is not considered as practical to this
Novel limitation.And throughout the drawings, the same reference numbers will be used to refer to the same parts.In the accompanying drawings:
Fig. 1 is a kind of spatial remotely sensed imaging semi physical based on sand table motor pattern involved in the utility model embodiment
The structural schematic diagram of emulation platform.
Specific embodiment
Exemplary embodiments of the present disclosure are described in more detail below with reference to accompanying drawings.Although showing the disclosure in attached drawing
Exemplary embodiment, it being understood, however, that may be realized in various forms the disclosure without should be by embodiments set forth here
It is limited.On the contrary, these embodiments are provided to facilitate a more thoroughly understanding of the present invention, and can be by the scope of the present disclosure
It is fully disclosed to those skilled in the art.
Fig. 1 diagrammatically illustrate a kind of space remote sensing based on sand table motor pattern of the utility model one embodiment at
As the structural schematic diagram of semi-physical simulation platform.Referring to Fig.1, the space based on sand table motor pattern of the utility model embodiment
Remotely sensed image semi-physical simulation platform can realize indoors, including kinematic system, camera load 101, solar simulator system and
Sand table 102, wherein
The kinematic system includes the gantry 103 being placed on the ground and the track that is slidably connected with described gantry 103
104;
The solar simulator system includes solar simulator 105 and solar light reflecting mirror 106, the solar light reflecting mirror
106 are vertically set on right above the solar simulator 105, and the solar simulator 105 is placed on the ground, the sand table
102 are arranged between the track 104, and the solar light reflecting mirror 106 is used for the light for emitting the solar simulator 105
It is reflected on the sand table 102.
The top at described gantry 103 is arranged in the camera load 101, as described gantry is mobile next on the track
Adjust distance of the camera load relative to the solar simulator and the sand table, with realize to the sand table 102 at
Picture.Wherein, the camera load includes infrared, EO-1 hyperion and low-light camera load, to simulate different remotely sensed image situations.
For the present embodiment by relationship that the camera load in remote sensing is vertically imaged at substar, physics indoors is imitative
It is replaced in true platform with horizontal imaging, so that solar simulator need not be set up in the sky, thereby reduces difficulty of construction, solved
In the conditional situation of story height, the problem that image-forming range is too short, breadth is too narrow, and then visible light can be supported indoors
Characteristic Simulation, target low-light-level performance simulation study carry out the remotely sensed image experiment and verifying of panchromatic, low-light etc..
In another embodiment of the utility model, the platform further includes three axis holders 107, the camera load
101 connects by the three axis holder 107 with described gantry 103, the camera load 101 by described gantry 103 vertically with/
Or the movement of horizontal movement and three axis holder, 107 pitching and/or rotation, with realize to the multi-angle of the sand table at
Picture.
For the present embodiment by relationship that the camera load in remote sensing is vertically imaged at substar, physics indoors is imitative
It is replaced in true platform with horizontal imaging, so that solar simulator need not be set up in the sky, thereby reduces difficulty of construction, increased
The angle of light propagation distance and variation, increases the area of hot spot, solves in the conditional situation of story height, at
The image distance problem too narrow from too short, breadth, and then realizing can support visible light characteristic emulation, target low-light-level performance to emulate indoors
The remotely sensed image experiment and verifying of panchromatic, low-light etc. are carried out in research.
In this embodiment of the utility model, the platform further include: two-dimensional movement turntable 108, the two dimension are moved
Turn platform 108 sand table 102 is arranged between two rails of the track 104, for adjusting the rotation of the sand table 102
And/or pitching.
The utility model embodiment, consideration solar simulator are powerful device, should not be moved, by building optical path as far as possible
Optical path length is elongated, larger irradiation scene is obtained.Sand table is designed using dimensional turntable motion base, rotatable, pitching, in hot spot
The multi-angle irradiation to target and scene can be achieved in area;Load is installed on movable machinery arm by three axis holders, can basis
Demand cooperates solar simulator to carry out imaging test to target, and real by the movement of two-dimensional movement turntable and three axis holders
The imaging of existing more perspective.
In a specific embodiment of the utility model, the spatial remotely sensed imaging semi-physical simulation platform includes fortune
Dynamic system, camera load, three axis holders, solar simulator system and sand table system, in which:
1, kinematic system specifically includes:
1, gantry, two, track, in orbit, gantry can be moved in the vertical direction and the horizontal direction for nested gantry setting
Dynamic, in the utility model embodiment, described gantry is also possible to that the equipment such as the bracket for moving equally effect can be played, right
This, the utility model embodiment is not particularly limited.
2, camera load
Height is less than 40cm;Quantity is 3, and quality is less than 50kg, and in the utility model embodiment, camera load includes
Infrared, EO-1 hyperion and low-light camera load simulates different remotely sensed image situation to realize, specifically can be according to being realized
Imaging contexts select different camera load.
Wherein, low-ligth level camera be it is a kind of can under the light condition of the faint natural light such as moonlight, starlight or skylight,
Carry out the camera of remote scene shot.When low-ligth level camera is had by high-energy radiation, it can record what radiation conversion generated
Dim light as the advantages of, being widely used in the fields machine such as scouting and the detection of underwater weak target is by strong luminous power main lens, low-light
Pipe is moved as lens and the part such as the sensitive film with special emulsion layer forms.
EO-1 hyperion camera load is the camera being imaged using high light spectrum image-forming technology, and high light spectrum image-forming technology is to be based on
The image data technology of very more narrow-bands, it combines imaging technique with spectral technique, and the two-dimensional geometry for detecting target is empty
Between and one-dimensional spectral information, obtain continuous, narrow-band the image data of high spectral resolution.
3, three axis holder, length 30cm;Quantity is 1, can carry 50kg;
One end of three axis holders is provided with camera load, to realize the movement of camera pitching and rotation.
4, solar simulator system specifically includes:
1 solar simulator and reflecting mirror, solar simulator transmitting is light after reflecting mirror reflects, and can achieve irradiation
2.5 meters of spot size diameter, 6 degree of light ray parallel precision.
Solar simulator system, and can lead at the case where being used to simulate light intensity, light and the spectrum of the true sun
Cross the adjusting for increasing filter disc to realize light intensity.
5, sand table system
The two-dimensional movement turntable of sand table and support sand table, two-dimensional movement turntable is rotatable, can direction along ng a path it is mobile, and can
In sun light direction pitching movement.Dipmeter and inclined angle regulating mechanism are provided on two-dimensional movement turntable.Dipmeter is used for
Pitch angle is measured, inclined angle regulating mechanism is used for adjusting pitch angle.
Wherein, solar simulator is horizontally arranged onto ground, and sand table system is placed between the guide rails, can direction along ng a path shifting
Dynamic, the top at gantry is provided with a three axis holders, wherein one end of three axis holders is provided with camera load, and camera load is logical
The vertical and horizontal movement at gantry and the movement of three axis holders, the imaging of Lai Shixian multi-angle are crossed, solar simulator is existed by setting
Light is reflected on sand table by the reflecting mirror right above it, has elongated optical path length in this way, can get larger irradiation scene.
In the utility model embodiment, solar simulator is using the light radiation of artificial light source simulated solar, to overcome too
Solar irradiation is by time and climatic effect, and the disadvantages of solar global irradiance is not adjustable, and is increased instead by two secondary reflections
Distance is penetrated, the hot spot being irradiated on sand table is increased.
Camera it is load simulated be detection load on satellite, in the present embodiment, camera load and sand table can be passed through
It is mobile to adjust, realize vertical imaging of the camera load on sand table.
In order to enable the result of physical platform emulation experiment is closer with true experimental result, semi-physical simulation is being obtained
, can be again by increasing existing environmental data after the experimental data of platform, and be overlapped with analogue data, so that physical simulation
Result be more nearly true remote sensing system.
Wherein, the present embodiment will increase the angle of light propagation distance and variation by indoor reflection mirror, so that sun mould
Quasi- device need not be set up in the sky, thereby reduce difficulty of construction, increase the area of hot spot, be solved restricted in story height
In the case where, the problem that image-forming range is too short, breadth is too narrow, and by increasing two-dimensional movement turntable, it realizes to specific mesh
The irradiation of target multi-angle light and multi-angle imaging, and stable distance is good, and then realizes and support visible light characteristic indoors
The remotely sensed image experiment and verifying of panchromatic, low-light etc. are carried out in emulation, target low-light-level performance simulation study.
In the instructions provided here, numerous specific details are set forth.It is to be appreciated, however, that the utility model
Embodiment can be practiced without these specific details.In some instances, be not been shown in detail well known method,
Structure and technology, so as not to obscure the understanding of this specification.
Similarly, it should be understood that in order to simplify the disclosure and help to understand one or more in each utility model aspect
A, in the description above to the exemplary embodiment of the utility model, each feature of the utility model is divided together sometimes
Group is into single embodiment, figure or descriptions thereof.However, the method for the disclosure should not be construed to reflect following meaning
Figure: the requires of the utility model features more more than feature expressly recited in each claim i.e. claimed.
More precisely, as reflected in the following claims, it is in terms of utility model single less than disclosed above
All features of embodiment.Therefore, it then follows thus claims of specific embodiment are expressly incorporated in the specific embodiment party
Formula, wherein separate embodiments of each claim as the utility model itself.
Those skilled in the art will understand that can be carried out adaptively to the module in the equipment in embodiment
Change and they are arranged in one or more devices different from this embodiment.It can be the module or list in embodiment
Member or component are combined into a module or unit or component, and furthermore they can be divided into multiple submodule or subelement or
Sub-component.Other than such feature and/or at least some of process or unit exclude each other, it can use any
Combination is to all features disclosed in this specification (including adjoint claim, abstract and attached drawing) and so disclosed
All process or units of what method or apparatus are combined.Unless expressly stated otherwise, this specification is (including adjoint power
Benefit require, abstract and attached drawing) disclosed in each feature can carry out generation with an alternative feature that provides the same, equivalent, or similar purpose
It replaces.
In addition, it will be appreciated by those of skill in the art that although some embodiments in this include institute in other embodiments
Including certain features rather than other feature, but the combination of the feature of different embodiment means to be in the utility model
Within the scope of and form different embodiments.For example, in the following claims, embodiment claimed is appointed
Meaning one of can in any combination mode come using.
The various component embodiments of the utility model can be implemented in hardware, or on one or more processors
The software module of operation is realized, or is implemented in a combination thereof.
The utility model is limited it should be noted that above-described embodiment illustrates rather than the utility model,
And those skilled in the art can be designed alternative embodiment without departing from the scope of the appended claims.In right
In it is required that, any reference symbol between parentheses should not be configured to limitations on claims.Word "comprising" is not arranged
Except there are element or steps not listed in the claims.Word "a" or "an" located in front of the element does not exclude the presence of more
A such element.The utility model can be by means of including the hardware of several different elements and by means of properly programmed
Computer is realized.In the unit claims listing several devices, several in these devices can be by same
One hardware branch embodies.The use of word first, second, and third does not indicate any sequence.It can be by these lists
Word is construed to title.
Claims (4)
1. a kind of spatial remotely sensed imaging semi-physical simulation platform based on sand table motor pattern, which is characterized in that including kinetic system
System, camera load, solar simulator system and sand table;
The kinematic system includes the gantry being placed on the ground and the track that is slidably connected with described gantry;
The solar simulator system includes solar simulator and solar light reflecting mirror, and the solar light reflecting mirror is vertically set on
Right above the solar simulator, the solar simulator is placed on the ground, and the sand table is placed between the track, institute
Solar light reflecting mirror is stated for the light that the solar simulator emits to be reflected into the sand table;
The top at described gantry is arranged in the camera load, moves on the track with described gantry and adjusts the phase
Distance of the airborne lotus relative to the solar simulator and the sand table, to realize the imaging to the sand table.
2. the spatial remotely sensed imaging semi-physical simulation platform according to claim 1 based on sand table motor pattern, feature
It is, further includes three axis holders, the camera load is connect by the three axis holder with described gantry, and the camera load is logical
The movement of vertical described gantry and/or horizontal movement and the three axis holder pitching and/or rotation is crossed, to realize to described
The multi-angle of sand table is imaged.
3. the spatial remotely sensed imaging semi-physical simulation platform according to claim 1 based on sand table motor pattern, feature
It is, further includes two-dimensional movement turntable, the sand table is arranged between the track two-dimensional movement turntable, for adjusting
The rotation and/or pitching of the sand table.
4. the spatial remotely sensed imaging semi-physical simulation according to claim 1-3 based on sand table motor pattern is flat
Platform, which is characterized in that the camera load includes infrared, EO-1 hyperion and low-light camera load, to simulate different remotely sensed image
Situation.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2018100552081 | 2018-01-19 | ||
CN201810055208 | 2018-01-19 |
Publications (1)
Publication Number | Publication Date |
---|---|
CN209248859U true CN209248859U (en) | 2019-08-13 |
Family
ID=64640660
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810739564.5A Active CN109036010B (en) | 2018-01-19 | 2018-07-06 | Space remote sensing imaging semi-physical simulation platform based on sand table movement mode |
CN201821075372.0U Expired - Fee Related CN209248859U (en) | 2018-01-19 | 2018-07-06 | A kind of spatial remotely sensed imaging semi-physical simulation platform based on sand table motor pattern |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201810739564.5A Active CN109036010B (en) | 2018-01-19 | 2018-07-06 | Space remote sensing imaging semi-physical simulation platform based on sand table movement mode |
Country Status (1)
Country | Link |
---|---|
CN (2) | CN109036010B (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109036010A (en) * | 2018-01-19 | 2018-12-18 | 北京市遥感信息研究所 | A kind of spatial remotely sensed imaging semi-physical simulation platform based on sand table motor pattern |
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 |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110686776B (en) * | 2019-10-09 | 2021-05-04 | 北京航空航天大学 | Indoor hyperspectral remote sensing imaging simulation device and method |
CN112631145B (en) * | 2020-11-20 | 2022-05-17 | 福州大学 | Semi-physical simulation system for unmanned aerial vehicle vision combined navigation test |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN100432628C (en) * | 2007-03-16 | 2008-11-12 | 北京航空航天大学 | Converting method and device for measuring daturm of sun sensor |
EP2667412A1 (en) * | 2007-04-18 | 2013-11-27 | Invisage Technologies, INC. | Materials, systems and methods for optoelectronic devices |
CN101713802B (en) * | 2009-11-13 | 2011-08-17 | 航天东方红卫星有限公司 | Fault on-line repairing method for satellite power supply and distribution test system |
CN102589849A (en) * | 2012-01-09 | 2012-07-18 | 上海大学 | Solar collecting and reflecting mirror surface fast performance assessment device and method |
CN102789240B (en) * | 2012-08-08 | 2014-10-15 | 中国科学院长春光学精密机械与物理研究所 | Device and method for simulating solar illumination with autoregulative azimuth angle |
CN102789237B (en) * | 2012-08-08 | 2015-06-10 | 中国科学院长春光学精密机械与物理研究所 | Device and method for simulating sun illumination by manually adjusting azimuth angle |
KR102088685B1 (en) * | 2012-12-19 | 2020-03-13 | 바스프 에스이 | Detector for optically detecting at least one object |
JP2014135365A (en) * | 2013-01-09 | 2014-07-24 | Solarflame Corp | Sunbeam condensation power generation device |
US9243776B1 (en) * | 2013-08-05 | 2016-01-26 | The Boeing Company | Solar simulator and method for solar simulation |
CN103438830A (en) * | 2013-09-09 | 2013-12-11 | 北京首航艾启威节能技术股份有限公司 | Solar energy condenser detection apparatus and detection method thereof |
CN103884520B (en) * | 2014-01-14 | 2015-08-19 | 北京控制工程研究所 | A kind of lunar surface topography and geomorphology simulator manufacture method |
CN104570764A (en) * | 2014-12-05 | 2015-04-29 | 中国运载火箭技术研究院 | Verification platform for airborne target indicating system |
US9689540B2 (en) * | 2015-05-05 | 2017-06-27 | The Boeing Company | Optical modifications for changing power density of solar simulator systems |
CN105242570A (en) * | 2015-10-12 | 2016-01-13 | 哈尔滨工业大学 | Aircraft-to-sun relationship ground simulation device |
CN106054160A (en) * | 2016-06-30 | 2016-10-26 | 上海宇航***工程研究所 | Integrated testing system for dynamic characteristics of visible light scattering and laser scattering of space target |
CN109036010B (en) * | 2018-01-19 | 2023-10-17 | 北京市遥感信息研究所 | Space remote sensing imaging semi-physical simulation platform based on sand table movement mode |
-
2018
- 2018-07-06 CN CN201810739564.5A patent/CN109036010B/en active Active
- 2018-07-06 CN CN201821075372.0U patent/CN209248859U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109036010A (en) * | 2018-01-19 | 2018-12-18 | 北京市遥感信息研究所 | A kind of spatial remotely sensed imaging semi-physical simulation platform based on sand table motor pattern |
CN109036010B (en) * | 2018-01-19 | 2023-10-17 | 北京市遥感信息研究所 | Space remote sensing imaging semi-physical simulation platform based on sand table movement mode |
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 |
Also Published As
Publication number | Publication date |
---|---|
CN109036010A (en) | 2018-12-18 |
CN109036010B (en) | 2023-10-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN209248859U (en) | A kind of spatial remotely sensed imaging semi-physical simulation platform based on sand table motor pattern | |
CN209248860U (en) | A kind of spatial remotely sensed imaging semi-physical simulation platform based on uniform zoom mode | |
CN113014906B (en) | 3D scene reconstruction method, system and computer program storage medium | |
CN106226759B (en) | Tracking stability testing device and method | |
CN103913737B (en) | Space Object Visible scatters dynamical property test system | |
CN109073376A (en) | The imaging of the 3-D based on LIDAR is carried out with the exposure intensity of variation | |
Jain et al. | Recent developments in the ROAMS planetary rover simulation environment | |
CN101251440B (en) | Dynamic goal simulator | |
CN105573328A (en) | Dynamic parameter calibration device of optical tracking/sighting pointing system and use method of dynamic parameter calibration device | |
CN104849023A (en) | High-precision multiband dynamic object simulator apparatus | |
CN104034697B (en) | A kind of assay device manufacturing surface roughness affect laser measurement performance and method | |
CN113176184A (en) | Simulation device for sea surface target pBRDF measurement and use method thereof | |
CN111025032A (en) | Aerial beam measuring system and method based on lift-off platform | |
CN109445310A (en) | A kind of infrared imaging guidance hardware-in-the-loop system and method | |
CN209248858U (en) | A kind of spatial remotely sensed imaging semi-physical simulation platform based on the tilting mode of sand table | |
CN115828616A (en) | Deep space infrared micro-motion target model construction method and imaging simulation system | |
CN115392009A (en) | Full-function complex scene generation software architecture | |
CN201173855Y (en) | Dynamic target generator | |
Piccinin et al. | ARGOS: Calibrated facility for Image based Relative Navigation technologies on ground verification and testing | |
CN106840606B (en) | A kind of car light PES projecting unit light gathering reflector analyzer | |
CN114593725B (en) | Tracking precision testing device and method for photoelectric tracker | |
CN104596416B (en) | Experimental measurement method and measurement apparatus that laser interacts with space junk | |
Wu et al. | Research on a wide-angle diagnostic method for shock wave velocity at SG-III prototype facility | |
CN114088358B (en) | Testing system and testing evaluation system for on-orbit imaging of space camera | |
CN114088359B (en) | Testing method for imaging performance of space camera and ground comprehensive simulation testing system |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
GR01 | Patent grant | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20190813 Termination date: 20200706 |
|
CF01 | Termination of patent right due to non-payment of annual fee |