CN1693922A - Combined measuring device using machine interference synthetic aperture radar base line - Google Patents
Combined measuring device using machine interference synthetic aperture radar base line Download PDFInfo
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- CN1693922A CN1693922A CNA200510069053XA CN200510069053A CN1693922A CN 1693922 A CN1693922 A CN 1693922A CN A200510069053X A CNA200510069053X A CN A200510069053XA CN 200510069053 A CN200510069053 A CN 200510069053A CN 1693922 A CN1693922 A CN 1693922A
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Abstract
The invention discloses an assembled device for detecting the plane-carried intervening composing aperture radar baseline. A rigid platform is installed on the bottom of a plane. There are two digital cameras, two laser range finder and an inertia detector. In the meanwhile, each intervening synthetic aperture radar antenna has several obvious LBD signs. These two cameras lenses face LBD signs on the antennas separately. The two cameras, two laser range finder and the inertia detector are all linked with the control processor, and for communication. The digital cameras and the laser range finder measure the moment position and pose of the intervening composing aperture radar antenna while the inertia detector measures the position and pose of the platform with the camera and the laser range finder. These three aspects unite together to realize the dynamic measurement of the interference synthetic aperture radar two-antenna.
Description
Technical field
The present invention relates to the combination metering device of a kind of airborne Interference synthetic aperture radar (interference SAR) baseline, relate in particular to a kind of two digital cameras, two laser range finders and Inertial Measurement Unit (IMU) of utilizing, to the position and the attitude of two radar receiving antennas hanging the interference synthetic aperture radar (interference SAR) under aircraft wing carry out accurately, the composite set of kinetic measurement.
Background technology
The system that the baseline of interference synthetic aperture radar (InSAR) the is carried out kinetic measurement space shuttle that mainly contains the U.S. and Germany's cooperation carries interference SAR system (SRTM) and U.S. GeoSAR airborne interference SAR system at present.
60 meters of the length of SRTM interference baseline, measuring system is made up of GPS location, inertial reference unit, star tracker, electronic distance measuring instrument, target tracker.The location of track mainly is to realize that with gps system bearing accuracy is better than 1m, and the main antenna attitude is measured by star tracker and inertial reference unit.Target tracker is a key device of measuring base linc motion, and it follows the tracks of three LEDs that are positioned on the outside antenna with the high precision camera.Five degree of freedom in the six-freedom degree of energy measurement outside antenna, another degree of freedom of outside antenna, promptly base length utilizes the electronic distance instrument to measure.
The baseline precision measurement apparatus of GeoSAR comprises two of inertial navigation unit, laser baseline measuring system and DGPS Receiver composition.And laser baseline measuring system comprises 5 laser range finders, 8 cameras, 5 wing gondola reverberators and 8 LED signs.Each side lay 4 cameras and 4 LED signs at fuselage, accurately measure the angle at LED sign center with camera; Lay a stadimeter on the radar antenna, all the other 4 are laid in respectively about fuselage, respectively to two reflecting prism measuring distances; Angle value and distance value are combined, calculate the three-dimensional coordinate of 1 point on each antenna and the two-dimensional coordinate of two points thus, utilize three-dimensional point to calculate base length, utilize two-dimensional points can calculate the orientation of baseline simultaneously.
Apparatus of the present invention are installed in two antennas of airborne Interference synthetic aperture radar (interference SAR) under the left and right sides wing of aircraft, use for radar emission and reception wireless signal.Still do not utilize it to do other purposes at present.
Summary of the invention
The combination metering device that the purpose of this invention is to provide a kind of machine interference synthetic aperture radar base line, two antennas that utilize existing airborne Interference synthetic aperture radar (interference SAR) are as measuring object, through synchronous data sampling, measure and calculate and obtain the accurately dynamic baseline of interference synthetic aperture radar (interference SAR).
For achieving the above object, technical solution of the present invention provides a kind of combination metering device of machine interference synthetic aperture radar base line, comprise two receiving antennas of interference synthetic aperture radar, platform, two digital cameras, two laser range finders, Inertial Measurement Unit and a processor controls, the ventral of its aircraft is installed a rigid platfor down, on platform, be installed with two digital cameras, two laser range finders and an Inertial Measurement Unit, on two antennas, settle several tangible LED markers simultaneously respectively;
LED marker on two antennas about the camera lens of two digital cameras faces toward respectively;
Two digital cameras, two laser range finders and Inertial Measurement Unit all electrically connect with processor controls, and carry out signal and communication.
Described combination metering device, the light emitting diode of settling respectively on its described two antennas is at least three.
Described combination metering device, it gathers the image of two receiving antennas, the measuring distance of laser range finder and the data of Inertial Measurement Unit by the center processor controls, realizes accurate kinetic measurement to the interference synthetic aperture radar baseline through Combined Treatment afterwards.
Described combination metering device, the LED marker of installing on its described receiving antenna, used the fixedly geometric relationship between these monumented points, the separate unit digital camera is measured the three-dimensional position of a receiving antenna in the digital camera coordinate system, adopt the collinearity equation of close-range photogrammetry, the Three-Dimensional Dynamic of receiving antenna that achieves a butt joint is measured.
Described combination metering device, its described laser range finder and digital camera synchronous acquisition data, trigger the laser pulse emission of the shutter of digital camera and laser range finder by a center processor controls, make the view data that digital camera obtains and the strictness coupling of laser ranging data.
Described combination metering device, its described two digital cameras and two laser range finder measurement data realize data fusion closely, utilize laser range finder distance to the high precision characteristic and digital camera measure on the plane to high precision, characteristic fast, realize that the complete three-dimensional high-precision of two receiving antennas is measured.
Described combination metering device, its described processor controls, position vector according to the digital camera center and the Inertial Measurement Unit center of indoor standardization, adopt the geometric transformation principle, the Inertial Measurement Unit data and digital camera, the laser range finder measurement data that obtain are carried out Combined Treatment, calculate the absolute position of receiving antenna under world geodetic system.
Description of drawings
Fig. 1 is the combination metering device scheme of installation of machine interference synthetic aperture radar base line of the present invention;
Fig. 2 is each parts annexation figure of combination metering device of machine interference synthetic aperture radar base line of the present invention.
Embodiment
Two antennas that the present invention is directed to existing airborne Interference synthetic aperture radar (interference SAR) are installed in the situation under the aircraft wing, have invented the device of following two the receiving antenna exact positions of a kind of kinetic measurement wing.Integrated two digital cameras of this device, two laser range finders and an Inertial Measurement Unit (IMU).
Digital camera and laser range finder are measured the instantaneous position and the attitude of interference synthetic aperture radar (interference SAR) antenna, Inertial Measurement Unit (IMU) is measured the position and the attitude of digital camera and laser range finder place platform, and the three combines and finally realizes the kinetic measurement of interference synthetic aperture radar (interference SAR) double antenna.
Apparatus of the present invention are according to the operation characteristic of low-to-medium altitude aircraft, integrated use the principle and the technology of digital close range photogrammetry and Inertial Measurement Unit (IMU), the composition of system and installing as shown in Figure 1.Two receiving antennas 5,5a of interference synthetic aperture radar (interference SAR) mount in aircraft both sides wing below, the ventral of aircraft is installed a rigid platfor 1 down, on this platform 1, be installed with two digital cameras 2,2a, two laser range finders 3,3a and Inertial Measurement Units (IMU) 4 are simultaneously settled 3 tangible light emitting diodes (LED), 6 signs respectively on two antennas 5 of synthetic aperture radar (SAR), 5a.Two antennas 5 about the camera lens of two digital cameras 2,2a faces toward respectively, 6 signs of the light emitting diode on the 5a.
During apparatus of the present invention work, by digital camera 2,2a measures light emitting diode (LED) 6 signs that are laid on the receiving antenna, while laser range finder 3,3a measures platform 1 and antenna 5 in real time synchronously, accurate distance between the 5a, adopt the collinearity equation of close-range photogrammetry to calculate two receiving antennas 5, the instantaneous position of 5a and attitude, Inertial Measurement Unit (IMU) 4 is measured digital camera 2 simultaneously, the exact position and the attitude of 2a place platform 1, concrete annexation is referring to Fig. 2, wherein, each parts on the platform 1: two digital cameras 2,2a, two laser range finders 3,3a and Inertial Measurement Unit (IMU) 4 all electrically connects with processor controls 7, and carries out signal and communication.Processor controls 7 is located in the cabin.
Digital camera 2 on the platform 1,2a can accurately measure receiving antenna 5,5a is at digital camera 2, position and attitude under the 2a coordinate system (local coordinate), because at receiving antenna 5, post 3 light emitting diodes (LED), 6 characteristic indications point on the 5a respectively, these monumented points have carried out accurate demarcation and measurement indoor in advance, with they as the constraint and the reference mark, while laser range finder 3,3a can provide platform 1 and antenna 5 again, distance between the 5a, according to the close-range photogrammetry principle, adopt collinearity equation, just can calculate receiving antenna 5, the 5a center is at digital camera 2, coordinate under the 2a coordinate system, and this coordinate information passed to processor controls 7.Inertial Measurement Unit on the platform 1 (IMU) 4 can accurately be measured the position and the attitude of digital camera 2,2a and laser range finder 3,3a place platform 1, and the position and the attitude information of platform 1 are passed to processor controls 7.Processor controls 7 just can be converted into the digital camera local coordinate system world geodetic system of the overall situation by the calculating of lever arm, thereby obtain two receiving antennas 5, exact position and the attitude of 5a center under the earth coordinates of the WGS84 whole world, provide the dynamic base measurement result of interference synthetic aperture radar (interference SAR).
Claims (4)
1. the combination metering device of a machine interference synthetic aperture radar base line, comprise two receiving antennas of interference synthetic aperture radar, a platform, two digital cameras, two laser range finders, an Inertial Measurement Unit and a center processor controls, it is characterized in that, the ventral of aircraft is installed a rigid platfor down, fixed installation two digital cameras, two laser range finders and Inertial Measurement Unit on this platform settled at least three tangible LED markers simultaneously respectively on two antennas;
Two radar antennas about the camera lens of two digital cameras faces toward respectively comprise the LED marker on the antenna in the visual field;
Two digital cameras, two laser range finders and Inertial Measurement Unit all electrically connect with the center processor controls, and carry out signal and communication.
2. combination metering device as claimed in claim 1, it is characterized in that, described laser range finder and digital camera synchronous acquisition data, trigger the laser pulse emission of the shutter and the laser range finder of digital camera by a processor controls, guarantee the laser ranging hot spot can with light emitting diode imaging simultaneously, make view data and the laser ranging data strict synchronism that digital camera obtains.
3. combination metering device as claimed in claim 1 or 2, it is characterized in that, come data and the digital camera images and the laser ranging data of synchronous acquisition Inertial Measurement Unit by the center processor controls, realize accurate kinetic measurement the interference synthetic aperture radar baseline through Combined Treatment afterwards.
4. combination metering device as claimed in claim 1 or 2, it is characterized in that, position vector according to the digital camera center and the Inertial Measurement Unit center of indoor standardization, adopt the geometric transformation principle, Inertial Measurement Unit data and digital camera, the laser range finder measurement data of gathering are carried out Combined Treatment, calculate the absolute three-dimensional position of radar receiving antenna under world geodetic system.
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| CN101241011B (en) * | 2007-02-28 | 2010-07-14 | 北京北科天绘科技有限公司 | High precision positioning and posture-fixing device on laser radar platform and method |
| CN101548198B (en) * | 2006-12-11 | 2012-06-20 | 艾利森电话股份有限公司 | A sar radar system and a method relating thereto |
| CN102749927A (en) * | 2012-07-20 | 2012-10-24 | 常州大学 | System for pilotless plane to automatically avoid barrier and avoiding method of system |
| CN102906601A (en) * | 2010-03-01 | 2013-01-30 | 克里斯多夫·I·莫伊尔 | A gradiometer |
| CN103323855A (en) * | 2012-03-22 | 2013-09-25 | 中国科学院电子学研究所 | Method for obtaining accuracy of reference line dynamic measurement system |
| CN103576145A (en) * | 2012-07-30 | 2014-02-12 | 中国科学院电子学研究所 | System and imaging method for airborne synthetic aperture laser radar |
| CN104155635A (en) * | 2014-08-23 | 2014-11-19 | 中国科学院成都生物研究所 | Ground penetrating radar single-channel electromagnetic spectrum three-dimensional positioning method |
| CN104269078A (en) * | 2014-09-23 | 2015-01-07 | 苏州天益航空科技有限公司 | Method for collision detection for agricultural plant protection unmanned aerial vehicle |
| CN105716627A (en) * | 2016-02-05 | 2016-06-29 | 中国科学院国家空间科学中心 | Concentric circle evenly-distributed interference base line arrangement method for CCD calibration |
| CN106371096A (en) * | 2016-05-25 | 2017-02-01 | 中国科学院遥感与数字地球研究所 | Airborne double antenna InSAR three-dimensional conformational model construction method |
| CN107102329A (en) * | 2017-04-17 | 2017-08-29 | 王辉 | Ka wave bands TOPS InSAR systems and its method of work |
| CN108375383A (en) * | 2018-02-22 | 2018-08-07 | 北京航空航天大学 | The airborne distribution POS flexibility base line measurement method and apparatus of polyphaser auxiliary |
| CN109323659A (en) * | 2018-09-29 | 2019-02-12 | 北京菲斯罗克光电技术有限公司 | A kind of airborne synthetic aperture radar baseline length measurement method and device |
| CN110068833A (en) * | 2019-05-05 | 2019-07-30 | 中国科学院电子学研究所 | A kind of synthetic aperture laser radar imaging method, instrument and system |
| CN110068817A (en) * | 2019-05-07 | 2019-07-30 | 中国科学院电子学研究所 | A kind of topographic mapping method, instrument and system based on laser ranging and InSAR |
| CN112070841A (en) * | 2020-07-01 | 2020-12-11 | 北京中科原动力科技有限公司 | Rapid combined calibration method for millimeter wave radar and camera |
| CN114993243A (en) * | 2022-08-04 | 2022-09-02 | 深圳粤讯通信科技有限公司 | Antenna attitude monitoring and early warning system based on Internet of things |
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| ITMI991154A1 (en) * | 1999-05-25 | 2000-11-25 | Milano Politecnico | PROCEDURE FOR RADAR MEASUREMENTS OF DISPLACEMENT OF URBAN PLANES AND SLIM ZONES |
| CN1156710C (en) * | 2000-09-25 | 2004-07-07 | 中国科学院空间科学与应用研究中心 | Real-time ground processing system for synthetic aperture imaging radar |
| CN1303431C (en) * | 2002-12-13 | 2007-03-07 | 中国科学院电子学研究所 | Airborne synthetic aperture radar surveying area positioning system |
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2005
- 2005-05-10 CN CNB200510069053XA patent/CN1329743C/en not_active Expired - Fee Related
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| CN101548198B (en) * | 2006-12-11 | 2012-06-20 | 艾利森电话股份有限公司 | A sar radar system and a method relating thereto |
| CN101241011B (en) * | 2007-02-28 | 2010-07-14 | 北京北科天绘科技有限公司 | High precision positioning and posture-fixing device on laser radar platform and method |
| US9140819B2 (en) | 2010-03-01 | 2015-09-22 | Christopher I. Moir | Gradiometer |
| CN102906601B (en) * | 2010-03-01 | 2017-04-05 | 克里斯多夫·I·莫伊尔 | Gravity gradiometer |
| CN102906601A (en) * | 2010-03-01 | 2013-01-30 | 克里斯多夫·I·莫伊尔 | A gradiometer |
| CN103323855B (en) * | 2012-03-22 | 2015-12-02 | 中国科学院电子学研究所 | A kind of precision acquisition methods of baseline dynamic measurement system |
| CN103323855A (en) * | 2012-03-22 | 2013-09-25 | 中国科学院电子学研究所 | Method for obtaining accuracy of reference line dynamic measurement system |
| CN102749927A (en) * | 2012-07-20 | 2012-10-24 | 常州大学 | System for pilotless plane to automatically avoid barrier and avoiding method of system |
| CN103576145A (en) * | 2012-07-30 | 2014-02-12 | 中国科学院电子学研究所 | System and imaging method for airborne synthetic aperture laser radar |
| CN103576145B (en) * | 2012-07-30 | 2016-01-20 | 中国科学院电子学研究所 | Airbome synthetic aperture laser radar system and formation method |
| CN104155635A (en) * | 2014-08-23 | 2014-11-19 | 中国科学院成都生物研究所 | Ground penetrating radar single-channel electromagnetic spectrum three-dimensional positioning method |
| CN104269078A (en) * | 2014-09-23 | 2015-01-07 | 苏州天益航空科技有限公司 | Method for collision detection for agricultural plant protection unmanned aerial vehicle |
| CN105716627B (en) * | 2016-02-05 | 2019-06-18 | 中国科学院国家空间科学中心 | It is a kind of for CCD calibration concentric circles be uniformly distributed interference baseline arrangement method |
| CN105716627A (en) * | 2016-02-05 | 2016-06-29 | 中国科学院国家空间科学中心 | Concentric circle evenly-distributed interference base line arrangement method for CCD calibration |
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| CN106371096B (en) * | 2016-05-25 | 2020-01-14 | 中国科学院遥感与数字地球研究所 | Airborne double-antenna InSAR three-dimensional configuration model construction method |
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| CN109323659A (en) * | 2018-09-29 | 2019-02-12 | 北京菲斯罗克光电技术有限公司 | A kind of airborne synthetic aperture radar baseline length measurement method and device |
| CN109323659B (en) * | 2018-09-29 | 2024-03-29 | 株洲菲斯罗克光电科技股份有限公司 | Method and device for measuring baseline length of airborne synthetic aperture radar |
| CN110068833A (en) * | 2019-05-05 | 2019-07-30 | 中国科学院电子学研究所 | A kind of synthetic aperture laser radar imaging method, instrument and system |
| CN110068833B (en) * | 2019-05-05 | 2021-10-29 | 中国科学院电子学研究所 | Synthetic aperture laser radar imaging method, instrument and system |
| CN110068817A (en) * | 2019-05-07 | 2019-07-30 | 中国科学院电子学研究所 | A kind of topographic mapping method, instrument and system based on laser ranging and InSAR |
| CN112070841A (en) * | 2020-07-01 | 2020-12-11 | 北京中科原动力科技有限公司 | Rapid combined calibration method for millimeter wave radar and camera |
| CN114993243A (en) * | 2022-08-04 | 2022-09-02 | 深圳粤讯通信科技有限公司 | Antenna attitude monitoring and early warning system based on Internet of things |
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