CN110133677A - A kind of integration navigation sensor - Google Patents
A kind of integration navigation sensor Download PDFInfo
- Publication number
- CN110133677A CN110133677A CN201910561196.4A CN201910561196A CN110133677A CN 110133677 A CN110133677 A CN 110133677A CN 201910561196 A CN201910561196 A CN 201910561196A CN 110133677 A CN110133677 A CN 110133677A
- Authority
- CN
- China
- Prior art keywords
- component
- light
- light path
- infrared
- path part
- 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.)
- Granted
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
- G01S17/02—Systems using the reflection of electromagnetic waves other than radio waves
- G01S17/06—Systems determining position data of a target
- G01S17/42—Simultaneous measurement of distance and other co-ordinates
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
- G01S17/66—Tracking systems using electromagnetic waves other than radio waves
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
- G01S17/88—Lidar systems specially adapted for specific applications
- G01S17/89—Lidar systems specially adapted for specific applications for mapping or imaging
Abstract
The invention discloses a kind of integrated navigation sensors, including lens assembly, short distance precision distance measurement machine, high-peak power laser, PSbox, electrically-controlled component；Lens assembly includes main support member, preceding light path part, rear light path part and outer cover part, and outer cover part is provided with above main support member, and preceding light path part is located at outer cover part left end, and outer cover part right end vertical direction is equipped with principal reflection mirror；Light path part is located at principal reflection mirror right end afterwards, and rear light path part includes infrared rear circuit unit, component prism, can see below light path part, and component prism is mounted on front side of principal reflection mirror, and infrared rear circuit unit is located above component prism；Light path part can be seen below and be located at component prism right end.It can be improved signal-to-noise ratio, image quality and position precision, guarantee stability and complete machine resonance frequency, reduce thermal control measure difficulty.
Description
Technical field
The present invention relates to space optics technical fields, and in particular to a kind of integration navigation sensor.
Background technique
Currently, deep space exploration has become the hot issue of international space flight field of detecting, the especially hair of China's aerospace industry
Exhibition is even more to advance by leaps and bounds, in order to meet the requirements at the higher level of spacecraft navigation sensor precision, optical navigation sensor calibration system
It is widely applied as optical navigation sensor ground calibration detection device.Existing society proposes optical system more tight
The requirement of lattice, examine etc. can capture especially for detection and fast and efficiently related objective, while realize high-precision
The tracking and measurement task of degree slowly develop into the main trend of current optical system development.And in order to obtain more horn of plenty
Detection data, and then devise new two waveband and multiband scheme.This system can be realized the efficient of multiple wave bands
Detection realizes efficient detection operation for the measured object of each classification.This is the irrealizable function of single optical system, because
This needs multiband duplex measurement.
Realize daytime with Visible Light Camera add it is infrared complex tracking is carried out to target, wave infrared cameras track mesh can be used at night
Mark, and with laser compound detection, it can be achieved that the mobile tenacious tracking of target and being accurately directed to for laser, and realize to target
Range measurement.
Summary of the invention
The present invention is in view of the above-mentioned problems, provide a kind of integrated navigation sensor, including lens assembly, short distance are in high precision
Range finder, high-peak power laser, PSbox, electrically-controlled component；The lens assembly include main support member, preceding light path part,
Light path part and outer cover part afterwards, the main support member top are provided with the outer cover part, and the preceding light path part is located at
Outer cover part left end, preceding light path part include outline border, secondary mirror, correction mirror, lens barrel, detector parts and preceding branch supporting element, institute
It states and is successively arranged correction mirror, secondary mirror and lens barrel inside outline border after from a left side, the detector parts are arranged in outer outer frame portion left end,
The preceding branch supporting element is located at outline border right end；Outer cover part right end vertical direction is equipped with principal reflection mirror, the rear light path part
Positioned at the principal reflection mirror right end, rear light path part includes infrared rear circuit unit, component prism, can see below light path part, institute
It states component prism to be mounted on front side of principal reflection mirror, is provided with block prism in component prism, the infrared rear circuit unit is located at
Above component prism, the light path part that sees below is located at component prism right end, the short distance precision distance measurement machine, peak value
Power laser diode and PSbox are arranged below main support member, and the electrically-controlled component is located at outer cover part bottom, electrically-controlled component packet
Include camera controller, secondary power supply, automatically controlled thermal control component.
Further, the preceding light path part, principal reflection mirror and rear light path part be in the same horizontal line.
Further, the outer cover part includes preceding cone, rear protective cover and lower protective cover, it is described after in protective cover
Part is upper chamber and lower chambers, is isolated among the upper chamber and lower chambers by multilayer aluminium film and nylon wire, institute
Lower protective cover is stated to be arranged below main support member.
Further, the outline border and the lens barrel junction are equipped with adjusting pad.
Further, the block prism has two pieces of triangular prisms to be spliced, it is seen that light and long wave infrared region
Light be incident on the light of block prism after light splitting, wherein LONG WAVE INFRARED light reflects upwards, be reflected into all the way it is infrared after
Light path part, in addition all the way after visible light-transmissive block prism, direct projection to Visible optical trains component.
Further, the infrared rear circuit unit includes that infrared lens component, infrared detector bracket and long wave are red
External detector, the infrared lens component are located above the component prism, are set in outside the infrared detector bracket infrared
Mirror element, the Long Wave Infrared Probe are arranged in infrared detector bracket right end.
Further, the visible light lens component is located at component prism right end, and the visible-light detector setting exists
Visible light lens component right end, it is seen that adjusting pad is equipped between optical detector and visible light lens component.
Advantages of the present invention: the present invention protects interior arrangement by outer cover part, realize to the inhibition of veiling glare with
And the protection of entire camera optical system is to inhibit, eliminate the outer stray light of the visual fields such as atmospheric scattering light, sunlight, can prevent one
Secondary, secondary veiling glare irradiates detector, improves detector signal-to-noise ratio, improves camera imaging quality, rear protective cover is divided into two chambers
Room guarantees that the Temperature Distribution of two components is mutually indepedent, does not interfere with each other；Preceding optical path component realizes the laser ranging of entire camera lens
Receiving unit, guarantees the position degree of sensitive detection parts image planes, and the accurate image planes position that controls is located at focal depth range center；Preceding optical path support
Bar acts the leading role the fixed support realized for preceding optical path component；High-peak power laser provides the laser that can determine spectral coverage；Closely
Accurate distance is obtained by calculation in laser range finder；Infrared rear circuit unit realizes infrared imaging；Light path part can be seen below to can
Light-exposed optical path is corrected, and realizes that visual light imaging makes to detect for controlling the coplanar precision of visible-light detector and position precision
Device image planes are located at focal depth range middle position, are conducive to improve camera lens thermal adaptability；Component prism will be seen that light and it is infrared into
Row light-splitting processing guarantees it will be seen that light and the light of long wave infrared region are reflected into Long Wave Infrared Probe respectively and visible light is visited
Survey device；Secondary power supply is whole system decorum stabilized power supply；Camera controller and automatically controlled thermal control component guarantee complete machine stability, whole
Machine resonance frequency reduces thermal control measure difficulty.
Other than objects, features and advantages described above, there are also other objects, features and advantages by the present invention.
Below with reference to figure, the present invention is described in further detail.
Detailed description of the invention
The attached drawing constituted part of this application is used to provide further understanding of the present invention, schematic reality of the invention
It applies example and its explanation is used to explain the present invention, do not constitute improper limitations of the present invention.
Fig. 1 is overall structure diagram of the invention；
Fig. 2 is the overall structure diagram of rear light path part of the invention；
Fig. 3 is the overall structure diagram of preceding light path part of the invention；
Fig. 4 is the structural schematic diagram of outer cover part of the invention；
Fig. 5 is side view of the invention；
Fig. 6 is the sectional view of the A-A of Fig. 5；
Fig. 7 is the sectional view of the B-B of Fig. 5；
Fig. 8 is optics whole design schematic diagram of the invention.
Appended drawing reference:
1 it is lens assembly, 2 be short distance precision distance measurement machine, 3 be high-peak power laser, 4 be PSbox, 5 is principal reflection
Mirror, 11 be main support member, 12 be preceding light path part, 121 be outline border, 122 be secondary mirror, 123 be lens barrel, 124 be detector portion
Part, 125 be preceding branch supporting element, 13 be rear light path part, 131 be infrared rear circuit unit, 132 be component prism, 133 for can
See below light path part, 134 block prisms, 135 be infrared lens component, 136 be infrared detector bracket, 137 be LONG WAVE INFRARED
Detector, 138 be visible light lens component, 139 be visible-light detector, 14 be outer cover part, 141 be preceding cone, 142 be
Protective cover, 143 are lower protective cover afterwards.
Specific embodiment
In order to make the objectives, technical solutions, and advantages of the present invention clearer, with reference to the accompanying drawings and embodiments, right
The present invention is further elaborated.It should be appreciated that described herein, specific examples are only used to explain the present invention, not
For limiting the present invention.
Embodiment 1
With reference to Fig. 1, Fig. 3, Fig. 5, Fig. 6 and Fig. 7, as shown in Fig. 1, Fig. 3, Fig. 5, Fig. 6 and Fig. 7, a kind of integration navigation sensor,
Including lens assembly 1, short distance precision distance measurement machine 2, high-peak power laser 3, PSbox4, electrically-controlled component；Lens assembly 1
Including main support member 11, preceding light path part 12, rear light path part 13 and outer cover part 14, it is provided with above main support member 11
Outer cover part 14, preceding light path part 12 are located at 14 left end of outer cover part, and preceding light path part 12 includes outline border 121, secondary mirror 122, rectifys
Telescope direct, lens barrel 123, detector parts 124 and preceding branch supporting element 125, preceding optical path component 12 are corrected including laser pick-off optical path
System and laser pickoff are realized the laser ranging receiving unit of entire camera lens, are successively arranged from a left side after inside outline border 121
Correction mirror, secondary mirror 122 and lens barrel 123, detector parts 124 are arranged in 121 outside left end of outline border, preceding branch supporting element 125
In 121 right end of outline border, preceding optical path support rod 125, which is mainly realized, supports the fixed of preceding light path part 12, outline border 121 and lens barrel
123 junctions are equipped with adjusting pad, and incidence makes 1064nm spectral coverage light wave in secondary mirror after principal reflection mirror 5 is reflected into secondary mirror 122
122 surface transmissions form preceding optical path across secondary mirror 122, after detector parts 124 are fixed by outline border 121, connect with lens barrel 123
It connects, as preceding 12 image planes position of light path part, outline border 121 and 123 junction of lens barrel are equipped with adjusting pad, for guaranteeing detector portion
The position degree of 124 image planes of part, the accurate image planes position that controls are located at focal depth range center, realize that laser radar receives setting for system
Meter；14 right end vertical direction of outer cover part is equipped with principal reflection mirror 5, and rear light path part 13 is located at 5 right end of principal reflection mirror, rear optical path portion
Part 13 includes infrared rear circuit unit 131, component prism 132, can see below light path part 133, and infrared rear circuit unit 131 includes
Infrared light path correction group and infrared remote receiver and it is infrared infrared light path is corrected, realize infrared imaging, component prism
132 are mounted on the front side of principal reflection mirror 5, are provided with block prism 134 in component prism 132, component prism 132 it will be seen that light with it is red
Outer to be divided, infrared rear circuit unit 131 is located at 132 top of component prism, it is seen that rear light path part 133 is located at component prism
132 right ends, it is seen that rear light path part 133 includes Visible optical trains correction group and visible light receiver, carries out school to visible light optical path
Just, realize that visual light imaging, preceding light path part 12, principal reflection mirror 5 and rear light path part 13 are in the same horizontal line, closely high
Precision range finder 2, high-peak power laser 3 and PSbox4 are arranged below main support member 11, short distance laser range finder
12 are obtained by calculation accurate distance, and high-peak power laser 3 provides the laser that can determine spectral coverage, and PSbox4 is provided into image quality
Amount, electrically-controlled component are located at 14 bottom of outer cover part, and electrically-controlled component includes camera controller, secondary power supply, automatically controlled thermal control component, electricity
Convenient the patching with each component of control component and cabling, secondary power supply are whole system decorum stabilized power supply.
With reference to Fig. 2, as shown in Fig. 2, infrared rear circuit unit 131 includes infrared lens component 135, infrared detector bracket
136 and Long Wave Infrared Probe 137, infrared lens component 135 is located at 132 top of component prism, outside infrared detector bracket 136
It is set in infrared mirror element 135, Long Wave Infrared Probe 137 is arranged in 136 right end of infrared detector bracket.
With reference to Fig. 4, as shown in figure 4, outer cover part 14 includes preceding cone 141, rear protective cover 142 and lower protective cover 143,
Outer cover part 14 realizes that preceding cone 141 primarily serves elimination to the inhibition of veiling glare and the protection of entire camera optical system
The effect of veiling glare, target being observed issue lightwave signal captured by optical system, by between optical element reflection or folding
The process penetrated eventually arrives at the image planes position of optical system, completes imaging process, setting aperture plate is suppression in outer cover part 14
System eliminates the outer stray light most efficient method of the visual fields such as atmospheric scattering light, sunlight, can prevent primary, secondary veiling glare from irradiating
Detector improves detector signal-to-noise ratio, improves camera imaging quality, is divided into upper chamber and lower chambers inside rear protective cover 142, point
Not Wei infrared rear circuit unit 131 and visible light lens component 138 protection is provided, since two-part operating temperature range has difference
Away from very greatly, it is isolated among upper chamber and lower chambers by multilayer aluminium film and nylon wire, guarantees the temperature point of two components
Cloth is mutually indepedent, does not interfere with each other, and lower protective cover 143 is arranged below main support member 11, and lower protective cover 143 is closely to swash
Protection is provided during ligh-ranging machine 2, peak value laser 3 and PSbox4, but for bottom electronics component provide mechanical interface and
Hot interface.
With reference to Fig. 8, as shown in figure 8, incident ray is after the reflection of principal reflection mirror 5, wherein visible light and long wave infrared region
Light through secondary mirror 122 reflection after, block prism 134 is incident on by 5 centre bore of principal reflection mirror, block prism 134 has two pieces
Triangular prism is spliced, and is mounted on 132 inside of component prism, is incident on the light of block prism 134 after light splitting, wherein
LONG WAVE INFRARED light reflects upwards, by after the infrared lens component 135 and component prism 132 that are connected with component prism 132
It is imaged at 137 image planes of Long Wave Infrared Probe, in addition all the way after visible light-transmissive block prism 134, by visible light lens
Component 138 is imaged, it is seen that set between optical detector 139 and visible light lens component 138 at 139 image planes of visible-light detector
There is adjusting pad, for controlling the coplanar precision of visible-light detector 139 and position precision, is located at 139 image planes of visible-light detector
Focal depth range middle position is conducive to improve camera lens thermal adaptability.
The key technical indexes of the invention, as shown in table 1.
1 the key technical indexes parameter of table
The index of multi-mode integration navigation sensor structure design:
A) main screw lift :≤5kg；
B) shape envelope :≤350mm × 200mm × 250mm；
C) resonance frequency: >=100Hz；
D) working life: >=3 years.
Embodiment 2
It unlike the first embodiment, is 1550nm in the spectral coverage light wave of 122 surface transmission of secondary mirror.
The working principle of the invention: daytime obtains target to the complex probe of target by visible light and infrared realization
Posture and position track target；By infrared imaging in the case that night or environmental condition are bad, realize detection to target with
Track；Etc. targets move to closely locate, by laser realization adjust the distance accurately measure, realize light-exposed high-resolution imaging, length
Camera integrated with the multi-mode of Airborne Lidar brake is imaged in the infrared refrigeration-type of wave.
The present invention protects interior arrangement by outer cover part 14, realizes inhibition and entire camera light to veiling glare
The protection of system is to inhibit, eliminate the outer stray light of the visual fields such as atmospheric scattering light, sunlight, can prevent primary, secondary veiling glare
Detector is irradiated, detector signal-to-noise ratio is improved, improves camera imaging quality, rear protective cover 142 is divided for two chambers, guarantee two
The Temperature Distribution of a component is mutually indepedent, does not interfere with each other；It is single to realize that the laser ranging of entire camera lens receives for preceding optical path component 125
Member, guarantees the position degree of sensitive detection parts image planes, and the accurate image planes position that controls is located at focal depth range center；Preceding optical path support rod 125
Act the leading role the fixed support realized for preceding optical path component 12；High-peak power laser 3 provides the laser that can determine spectral coverage；Closely
Accurate distance is obtained by calculation in laser range finder 2；Infrared rear circuit unit 131 realizes infrared imaging；Light path part can be seen below
133 pairs of visible light optical paths are corrected, and visual light imaging are realized, for controlling the coplanar precision of visible-light detector 139 and position
Precision makes detector image planes be located at focal depth range middle position, is conducive to improve camera lens thermal adaptability；Component prism 132 will
Visible light and infrared carry out light-splitting processing guarantee it will be seen that light and the light of long wave infrared region are reflected into LONG WAVE INFRARED spy respectively
Survey device 137 and visible-light detector 139；Secondary power supply is whole system decorum stabilized power supply；Camera controller and automatically controlled thermal control
Component guarantees complete machine stability, complete machine resonance frequency, reduces thermal control measure difficulty.
The foregoing is merely presently preferred embodiments of the present invention, is not intended to limit the invention, it is all in spirit of the invention and
Within principle, any modification, equivalent replacement, improvement and so on be should all be included in the protection scope of the present invention.
Claims (7)
1. it is a kind of integration navigation sensor, which is characterized in that including lens assembly (1), short distance precision distance measurement machine (2),
High-peak power laser (3), PSbox(4), electrically-controlled component；The lens assembly (1) includes main support member (11), preceding light
Circuit unit (12), rear light path part (13) and outer cover part (14), main support member (11) top are provided with the outer cover
Component (14), the preceding light path part (12) are located at outer cover part (14) left end, preceding light path part (12) include outline border (121),
Secondary mirror (122), correction mirror, lens barrel (123), detector parts (124) and preceding branch supporting element (125), the outline border (121) are interior
Portion is successively arranged correction mirror, secondary mirror (122) and lens barrel (123) from a left side after, and the detector parts (124) are arranged in outline border
(121) external left end, the preceding branch supporting element (125) are located at outline border (121) right end；Outer cover part (14) right end vertical direction
Equipped with principal reflection mirror (5), the rear light path part (13) is located at the principal reflection mirror (5) right end, and rear light path part (13) includes
Infrared rear circuit unit (131), can be seen below light path part (133) component prism (132), and the component prism (132) is mounted on
On front side of principal reflection mirror (5), it is provided with block prism (134) in component prism (132), infrared rear circuit unit (131) position
Above component prism (132), the light path part (133) that sees below is located at component prism (132) right end, and the short distance is high
Precision range finder (2), high-peak power laser (3) and PSbox(4) setting it is described automatically controlled below the main support member (11)
Component is located at outer cover part (14) bottom, and electrically-controlled component includes camera controller, secondary power supply, automatically controlled thermal control component.
2. integration navigation sensor according to claim 1, which is characterized in that the preceding light path part (12), master are anti-
Penetrate mirror (5) and rear light path part (13) in the same horizontal line.
3. integration navigation sensor according to claim 1, which is characterized in that the outer cover part (14) includes preceding screening
Light cylinder (141), rear protective cover (142) and lower protective cover (143), the rear protective cover (142) is internal to be divided into upper chamber and cavity of resorption
It is isolated among room, the upper chamber and lower chambers by multilayer aluminium film and nylon wire, lower protective cover (143) setting
Below main support member (11).
4. integration navigation sensor according to claim 1, which is characterized in that the outline border (121) and the lens barrel
(124) junction is equipped with adjusting pad.
5. integration navigation sensor according to claim 1, which is characterized in that the block prism (134) has two pieces
Triangular prism is spliced, it is seen that light and the light of long wave infrared region are incident on the light of block prism (134) by light splitting
Afterwards, wherein LONG WAVE INFRARED light reflects upwards, is reflected into infrared rear circuit unit (131) all the way, in addition visible light-transmissive all the way
After block prism (134), direct projection to Visible optical trains component (133).
6. integration navigation sensor according to claim 1, which is characterized in that the infrared rear circuit unit (131)
Including infrared lens component (135), infrared detector bracket (136) and Long Wave Infrared Probe (137), the infrared lens portion
Part (135) is located above the component prism (132), and infrared mirror element is set in outside the infrared detector bracket (136)
(135), the Long Wave Infrared Probe (137) is arranged in infrared detector bracket (136) right end.
7. integration navigation sensor according to claim 1, which is characterized in that described to see below light path part (133)
Including visible light lens component (138) and visible-light detector (139), the visible light lens component (138) is located at prism portion
Part (132) right end, the visible-light detector (139) are arranged in visible light lens component (138) right end, it is seen that optical detector
(139) adjusting pad is equipped between visible light lens component (138).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910561196.4A CN110133677B (en) | 2019-06-26 | 2019-06-26 | Integrated navigation sensor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910561196.4A CN110133677B (en) | 2019-06-26 | 2019-06-26 | Integrated navigation sensor |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110133677A true CN110133677A (en) | 2019-08-16 |
| CN110133677B CN110133677B (en) | 2020-12-04 |
Family
ID=67579568
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910561196.4A Active CN110133677B (en) | 2019-06-26 | 2019-06-26 | Integrated navigation sensor |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110133677B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116781168A (en) * | 2023-06-14 | 2023-09-19 | 蓝星光域(上海)航天科技有限公司 | Integrated laser communication terminal |
| CN116929374A (en) * | 2023-05-26 | 2023-10-24 | 北京控制工程研究所 | Earth sensor |
Citations (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5025149A (en) * | 1990-06-18 | 1991-06-18 | Hughes Aircraft Company | Integrated multi-spectral boresight target generator |
| EP0536833A1 (en) * | 1991-10-10 | 1993-04-14 | Koninklijke Philips Electronics N.V. | X-ray examination apparatus |
| JPH10333559A (en) * | 1997-05-29 | 1998-12-18 | Alpine Electron Inc | On-vehicle navigation device and map data storage medium |
| US20020140596A1 (en) * | 2001-03-28 | 2002-10-03 | Stolarczyk Gerald L. | Landmine locating system |
| US20050024624A1 (en) * | 2003-07-31 | 2005-02-03 | Gruhlke Russell W. | Speckle based sensor for three dimensional navigation |
| CN101236091A (en) * | 2008-01-31 | 2008-08-06 | 北京控制工程研究所 | Visual light navigation sensor |
| CN101275847A (en) * | 2007-03-29 | 2008-10-01 | 北京控制工程研究所 | Ultraviolet light imaging type autonomous navigation sensor system of low orbit spacecraft |
| CN102288178A (en) * | 2011-03-28 | 2011-12-21 | 南京航空航天大学 | Aerospace object middle-remote distance relative navigating device and navigating method thereof |
| CN102636818A (en) * | 2012-04-27 | 2012-08-15 | 清华大学 | Star tracking and composite grouping type earth gravitational field measurement system and method |
| CN102927982A (en) * | 2012-09-29 | 2013-02-13 | 哈尔滨工业大学 | Double-spectrum autonomous navigation sensor and design method of double-spectrum autonomous navigation sensor |
| CN103077502A (en) * | 2012-12-28 | 2013-05-01 | 北京控制工程研究所 | Star sensor star point denoising method |
| CN103278916A (en) * | 2013-04-10 | 2013-09-04 | 北京理工大学 | Laser and middle- and long-wavelength infrared common-aperture three-band imaging system |
| CN103438885A (en) * | 2013-08-27 | 2013-12-11 | 西北工业大学 | Three-channel polarized navigation sensor |
| EP2719990A1 (en) * | 2012-10-11 | 2014-04-16 | MBDA Deutschland GmbH | Device for optical target assignment and guidance of a missile |
| CN103743397A (en) * | 2013-12-18 | 2014-04-23 | 北京控制工程研究所 | Internal stray light eliminating star sensor |
| CN102866490B (en) * | 2012-09-27 | 2014-12-10 | 中国科学院西安光学精密机械研究所 | Optical imaging system for visible light waveband, medium-wave infrared waveband and long-wave infrared waveband |
| CN104482934A (en) * | 2014-12-30 | 2015-04-01 | 华中科技大学 | Multi-transducer fusion-based super-near distance autonomous navigation device and method |
| CN105910627A (en) * | 2016-07-08 | 2016-08-31 | 哈尔滨工业大学 | Dynamic simulator used for spatial visual navigation sensor |
| CN106767713A (en) * | 2016-11-22 | 2017-05-31 | 北京空间机电研究所 | A kind of multi-channel integrated active-passive composite mapping camera system |
| CN107299568A (en) * | 2017-06-16 | 2017-10-27 | 中铁工程设计咨询集团有限公司 | A kind of track dynamic measuring system and method |
| CN107883945A (en) * | 2017-10-11 | 2018-04-06 | 北京控制工程研究所 | It is a kind of to suppress angle star sensor without the sun |
| CN108957715A (en) * | 2018-09-19 | 2018-12-07 | 江苏无线电厂有限公司 | A kind of coaxial electro optical reconnaissance system |
| CN109060128A (en) * | 2018-07-13 | 2018-12-21 | 中国科学院光电研究院 | A kind of imaging spectrum system of visible light and short-wave infrared Shared aperture |
| CN109211223A (en) * | 2018-09-30 | 2019-01-15 | 北京控制工程研究所 | It is a kind of integrated close to measurement sensor and system |
| CN109655157A (en) * | 2018-12-29 | 2019-04-19 | 华中科技大学 | A kind of visible light-infared spectrum detection device and method |
| CN109900225A (en) * | 2019-04-24 | 2019-06-18 | 吉林大学 | A kind of superhigh precision angle measurement system |
-
2019
- 2019-06-26 CN CN201910561196.4A patent/CN110133677B/en active Active
Patent Citations (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5025149A (en) * | 1990-06-18 | 1991-06-18 | Hughes Aircraft Company | Integrated multi-spectral boresight target generator |
| EP0536833A1 (en) * | 1991-10-10 | 1993-04-14 | Koninklijke Philips Electronics N.V. | X-ray examination apparatus |
| JPH10333559A (en) * | 1997-05-29 | 1998-12-18 | Alpine Electron Inc | On-vehicle navigation device and map data storage medium |
| US20020140596A1 (en) * | 2001-03-28 | 2002-10-03 | Stolarczyk Gerald L. | Landmine locating system |
| US20050024624A1 (en) * | 2003-07-31 | 2005-02-03 | Gruhlke Russell W. | Speckle based sensor for three dimensional navigation |
| US7205521B2 (en) * | 2003-07-31 | 2007-04-17 | Avage Technologies Ecbu Ip (Singapore) Pte. Ltd. | Speckle based sensor for three dimensional navigation |
| CN101275847A (en) * | 2007-03-29 | 2008-10-01 | 北京控制工程研究所 | Ultraviolet light imaging type autonomous navigation sensor system of low orbit spacecraft |
| CN101236091A (en) * | 2008-01-31 | 2008-08-06 | 北京控制工程研究所 | Visual light navigation sensor |
| CN102288178A (en) * | 2011-03-28 | 2011-12-21 | 南京航空航天大学 | Aerospace object middle-remote distance relative navigating device and navigating method thereof |
| CN102636818A (en) * | 2012-04-27 | 2012-08-15 | 清华大学 | Star tracking and composite grouping type earth gravitational field measurement system and method |
| CN102866490B (en) * | 2012-09-27 | 2014-12-10 | 中国科学院西安光学精密机械研究所 | Optical imaging system for visible light waveband, medium-wave infrared waveband and long-wave infrared waveband |
| CN102927982A (en) * | 2012-09-29 | 2013-02-13 | 哈尔滨工业大学 | Double-spectrum autonomous navigation sensor and design method of double-spectrum autonomous navigation sensor |
| EP2719990A1 (en) * | 2012-10-11 | 2014-04-16 | MBDA Deutschland GmbH | Device for optical target assignment and guidance of a missile |
| CN103077502A (en) * | 2012-12-28 | 2013-05-01 | 北京控制工程研究所 | Star sensor star point denoising method |
| CN103278916A (en) * | 2013-04-10 | 2013-09-04 | 北京理工大学 | Laser and middle- and long-wavelength infrared common-aperture three-band imaging system |
| CN103438885A (en) * | 2013-08-27 | 2013-12-11 | 西北工业大学 | Three-channel polarized navigation sensor |
| CN103743397A (en) * | 2013-12-18 | 2014-04-23 | 北京控制工程研究所 | Internal stray light eliminating star sensor |
| CN104482934A (en) * | 2014-12-30 | 2015-04-01 | 华中科技大学 | Multi-transducer fusion-based super-near distance autonomous navigation device and method |
| CN105910627A (en) * | 2016-07-08 | 2016-08-31 | 哈尔滨工业大学 | Dynamic simulator used for spatial visual navigation sensor |
| CN106767713A (en) * | 2016-11-22 | 2017-05-31 | 北京空间机电研究所 | A kind of multi-channel integrated active-passive composite mapping camera system |
| CN107299568A (en) * | 2017-06-16 | 2017-10-27 | 中铁工程设计咨询集团有限公司 | A kind of track dynamic measuring system and method |
| CN107883945A (en) * | 2017-10-11 | 2018-04-06 | 北京控制工程研究所 | It is a kind of to suppress angle star sensor without the sun |
| CN109060128A (en) * | 2018-07-13 | 2018-12-21 | 中国科学院光电研究院 | A kind of imaging spectrum system of visible light and short-wave infrared Shared aperture |
| CN108957715A (en) * | 2018-09-19 | 2018-12-07 | 江苏无线电厂有限公司 | A kind of coaxial electro optical reconnaissance system |
| CN109211223A (en) * | 2018-09-30 | 2019-01-15 | 北京控制工程研究所 | It is a kind of integrated close to measurement sensor and system |
| CN109655157A (en) * | 2018-12-29 | 2019-04-19 | 华中科技大学 | A kind of visible light-infared spectrum detection device and method |
| CN109900225A (en) * | 2019-04-24 | 2019-06-18 | 吉林大学 | A kind of superhigh precision angle measurement system |
Non-Patent Citations (6)
| Title |
|---|
| FRANCESCO SANSONE 等: "Low-cost relative navigation sensors for miniature spacecraft and drones", 《2015 IEEE METROLOGY FOR AEROSPACE》 * |
| LI SHUANG 等: "Autonomous navigation and guidance scheme for precise and safe planetary landing", 《AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY》 * |
| XUEYING LV 等: "Improved Particle Swarm Optimization Algorithm Based on Last-Eliminated Principle and Enhanced Information Sharing", 《COMPUTATIONAL INTELLIGENCE AND NEUROSCIENCE》 * |
| 戴永江 等: "空间交会对接用激光雷达敏感器", 《激光与红外》 * |
| 李欣璐 等: "特定历元时刻星敏感器定姿", 《中国空间科学学会2013年空间光学与机电技术研讨会》 * |
| 王志国 等: "高轨卫星机热一体化星敏感器支架设计", 《航天器工程》 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN116929374A (en) * | 2023-05-26 | 2023-10-24 | 北京控制工程研究所 | Earth sensor |
| CN116929374B (en) * | 2023-05-26 | 2024-01-19 | 北京控制工程研究所 | Earth sensor |
| CN116781168A (en) * | 2023-06-14 | 2023-09-19 | 蓝星光域(上海)航天科技有限公司 | Integrated laser communication terminal |
Also Published As
| Publication number | Publication date |
|---|---|
| CN110133677B (en) | 2020-12-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| EP3457080B1 (en) | Surveying instrument | |
| CN109100876B (en) | Multi-optical-axis parallel adjusting device and multi-optical-axis parallel adjusting method | |
| CA2636381C (en) | Coordinate measurment apparatus | |
| CN108957715B (en) | Coaxial photoelectric reconnaissance system | |
| CN102803990B (en) | Tracking method and measuring system having a laser tracker | |
| EP1037014B1 (en) | Electric level | |
| CN101115970B (en) | Measuring device and method that operates according to the basic principles of confocal microscopy | |
| CN110487514A (en) | A kind of plain shaft parallelism calibration system of the multispectral photoelectric detecting system in aperture altogether | |
| CN101776516B (en) | Position detector-based dividing plane-sharing multispectral target | |
| CN104567668A (en) | Scanner for space measurement | |
| US8724104B2 (en) | Coarse and fine projective optical metrology system | |
| US20210025978A1 (en) | Coordinate measuring device having automatic target object recognition | |
| CN110133677A (en) | A kind of integration navigation sensor | |
| CN104603635A (en) | Laser tracker with hybrid imaging method for extending the measuring range | |
| CN110823527A (en) | Calibration method for optical axis of multi-sensor containing laser | |
| CN102334007B (en) | Leveling device and leveling method | |
| CN114236559A (en) | Common-aperture six-waveband imaging spectrum ranging optical system for low-slow small aircraft | |
| CN105510925A (en) | Laser tracker with warm air flow shield for measurement beam | |
| CN208350032U (en) | Coaxial transmitting-receiving detection device | |
| CA2213501A1 (en) | Displacement measurement apparatus and method | |
| CN109000584A (en) | Coaxial transmitting-receiving detection device | |
| EP4332630A1 (en) | Measuring device with tof sensor | |
| RU2746089C1 (en) | Detection device for optical and optoelectronic devices | |
| US11619582B2 (en) | Retroreflectometer for non-contact measurements of optical characteristics | |
| RU2529732C1 (en) | System for detecting objects |
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 | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20220928 Address after: Room 201, Building 5, Northwest District, Nano City, No. 99, Jinjihu Avenue, Suzhou Industrial Park, Suzhou Area, Wuzhong District Free Trade Pilot Zone, Suzhou City, Jiangsu Province, 215000 Patentee after: Suzhou jitianxingzhou Space Technology Co.,Ltd. Address before: 130000 No. 2699 Qianjin Street, Jilin, Changchun Patentee before: Jilin University |
|
| TR01 | Transfer of patent right |