CN104567653A - Method for measuring angle of inner frame of multi-frame pod by electric eddy-current transducer - Google Patents

Method for measuring angle of inner frame of multi-frame pod by electric eddy-current transducer Download PDF

Info

Publication number
CN104567653A
CN104567653A CN201410830428.9A CN201410830428A CN104567653A CN 104567653 A CN104567653 A CN 104567653A CN 201410830428 A CN201410830428 A CN 201410830428A CN 104567653 A CN104567653 A CN 104567653A
Authority
CN
China
Prior art keywords
inner frame
vortex sensor
current vortex
angle
alpha
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
Application number
CN201410830428.9A
Other languages
Chinese (zh)
Other versions
CN104567653B (en
Inventor
丁伟
朱娜
耿欣
丁祝顺
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
China Aerospace Times Electronics Corp
Beijing Aerospace Control Instrument Institute
Original Assignee
China Aerospace Times Electronics Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by China Aerospace Times Electronics Corp filed Critical China Aerospace Times Electronics Corp
Priority to CN201410830428.9A priority Critical patent/CN104567653B/en
Publication of CN104567653A publication Critical patent/CN104567653A/en
Application granted granted Critical
Publication of CN104567653B publication Critical patent/CN104567653B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Measurement Of Length, Angles, Or The Like Using Electric Or Magnetic Means (AREA)

Abstract

The invention discloses a method for measuring an angle of an inner frame of a multi-frame pod by an electric eddy-current transducer. The method comprises steps as follows: the electric eddy-current transducer and an induction steel disc are installed on a to-be-measured inner frame and an installation frame of the inner frame respectively; when the to-be-measured inner frame rotates relative to the installation frame, the distance between the electric eddy-current transducer and the induction steel disc is changed, and the electric eddy-current transducer outputs a voltage signal V related with distance change; the voltage signal output by the electric eddy-current transducer is subjected to filter and analog-digital conversion, and meanwhile, the distance h between the electric eddy-current transducer and the induction steel disc is calculated according to a scaling factor of the electric eddy-current transducer and an amplification coefficient of analog-digital conversion; the angle between the to-be-measured inner frame and the installation frame of the inner frame is calculated according to the distance h between the electric eddy-current transducer and the induction steel disc. The size and the weight of a multi-frame pod system can be reduced, the friction force can be reduced, and high-precision angle measurement can be realized.

Description

A kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle
Technical field
The present invention relates to a kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle, belong to many frameworks gondola control technology field.
Background technology
Photoelectric nacelle keeps its inside panel stable in motion process with rate stabilization principle, utilize load on platform (can by light video camera, thermal infrared imager, airborne laser range finder etc.) to obtain the information such as image, distance of target, complete the identification of target, follow the tracks of and locate.The fields such as Aerial photography, military surveillance, border patrols, searching rescue, safety law enforcement are widely used according to the outfit of load.The performance of photoelectric nacelle is mainly reflected in infrared, the detection range of visible ray and the range capability of laser instrument.These performances load self meet condition under, then determined by the lasting accuracy of photoelectric nacelle.At present, the lasting accuracy of external photoelectric nacelle can reach 3 differential of the arcs (be equivalent to 1 km target far away and only rock 3 millimeters), and corresponding range capability can reach 30 kms.And the lasting accuracy of domestic photoelectric nacelle is 25 differential of the arcs, range capability is 15 kms, and gap is larger.
Many frameworks photoelectric nacelle is the dominant form of electro-optical pod, refers to and utilizes inside and outside two-layer frame stability to same axle: outside framework resists windage, elementary vibration damping; Inner frame realizes higher lasting accuracy.When outside framework is identical, the lasting accuracy of inner frame determines the lasting accuracy of whole many frameworks photoelectric nacelle.Current many frameworks photoelectric nacelle inner frame both domestic and external all utilizes scrambler or rotary transformer device to take measurement of an angle.First, inner frame angle is little, be generally less than ± 3 °.And scrambler or rotary transformer are all-round measuring element, so the waste on volume, weight and range can be brought when utilizing above-mentioned device angle measurement.Secondly, all need corresponding axle head to support when scrambler and rotary transformer application, can friction be introduced, and friction force is the principal element affecting platform stable precision.A kind of many frameworks gondola inner frame angle high-precision measuring method that can reduce friction of current urgent need.
Summary of the invention
The technology of the present invention is dealt with problems and is: for the deficiencies in the prior art, provide a kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle, by adopting current vortex sensor and accurate computing in the inner frame of many frameworks photoelectric nacelle, obtain high-precision many frameworks gondola angle measurement.
Technical solution of the present invention:
A kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle:
Current vortex sensor and induction steel disc are installed on the installation frame of inner frame to be measured and this inner frame respectively;
When inner frame to be measured rotates relative to its installation frame, current vortex sensor changes relative to the distance of induction steel disc, and current vortex sensor exports and changes relevant voltage signal V to distance;
The voltage signal that current vortex sensor exports, by filtering and analog to digital conversion, simultaneously calculates current vortex sensor and induction steel disc distance h according to the scale factor of current vortex sensor and analog-to-digital amplification coefficient;
According to the distance h of current vortex sensor and induction steel disc, the angle between the installation frame calculating inner frame to be measured and this inner frame.
The installation site of described current vortex sensor is R apart from the length in the axle center of inner frame to be measured 1, described R 1for wherein L 1for the range of current vortex sensor, θ are the required angular range, the described R that measure 1under meeting the prerequisite of inequality, R 1value should be as far as possible close
Described calculating current vortex sensor and induction steel disc distance wherein, k 1represent the scale factor of current vortex sensor, n represents analog-to-digital figure place, and η represents analog-to-digital input voltage range.
The described distance h according to current vortex sensor and induction steel disc, the specific implementation of the angle beta between the installation frame calculating inner frame to be measured and this inner frame is as follows:
(4a) the angle α of the induction straight line at steel disc place and the axle center of inner frame to be measured and steel disc line is calculated:
α = arcsin ( 0.5 L 1 + L 3 R 1 )
Wherein, L 3represent that current vortex sensor distance perspective answers the minor increment of steel disc;
(4b) the angle α and distance h that obtain in step (4a) is utilized, the angle beta between the installation frame calculating inner frame to be measured and this inner frame:
β = arc cos ( 1 - c 2 + 2 c tan α - c tan α + tan 2 α 1 + tan 2 β )
Wherein, c = h 1 + tan 2 α R 1 .
Angle beta between described inner frame to be measured and the installation frame of this inner frame, when measuring accuracy requires lower, formula of reduction can be utilized to calculate, and formula of reduction is:
Described induction steel disc and the installation site of current vortex sensor can exchange, and are installed on the installation frame of inner frame to be measured and this inner frame respectively, the angle of the installation frame of inner frame to be measured and this inner frame β 1 = arccos ( 1 - c 1 2 + 2 c 1 tan α 1 - c 1 tan α 1 + tan 2 α 1 1 + tan 2 α 1 ) , Wherein α 1for the angle of the straight line at current vortex sensor place and the axle center of inner frame to be measured and current vortex sensor line;
The present invention is relative to the beneficial effect of prior art:
(1) means such as the present invention by adopting electric vortex sensor measuring angle in the inner frame of many frameworks photoelectric nacelle, the scrambler of the equal size adopted relative to prior art, can improve the inner frame angle-measurement accuracy of many frameworks gondola significantly.
(2) the present invention is relative to prior art, the current vortex sensor adopted without the need to installing turning axle separately, decrease between centers friction, improve many frameworks photoelectric nacelle lasting accuracy, reduce the volume of inner frame, weight simultaneously.
(3) the present invention sets up the coordinate system of current vortex sensor and induction steel disc, calculated by the position mathematical model and strict data of setting up two, solve the position relationship of current vortex sensor and induction steel disc, and then solve inner frame angle, improve the measuring accuracy of inner frame angle, improve the performance of many frameworks pod control system.
Accompanying drawing explanation
Fig. 1 is current vortex sensor of the present invention and induction steel disc composition schematic diagram;
Fig. 2 is the present invention's many frameworks gondola bearing wall and frame structure schematic layout pattern;
Fig. 3 is the position relationship schematic diagram of current vortex sensor of the present invention and induction steel disc and pitching frame;
Fig. 4 is that the present invention is along pitch axis direction current vortex sensor and the relative position relation schematic diagram responding to steel disc;
Fig. 5 is the angle calculation schematic diagram between the installation frame of the present invention's inner frame to be measured and this inner frame;
Fig. 6 is the numerical value corresponding relation figure of accurate angle of the present invention and rough angle and ADC value;
Fig. 7 is the numerical value corresponding relation figure of angle difference that the present invention is accurate and rough and ADC value.
Embodiment
Below in conjunction with accompanying drawing, principle of work of the present invention and the course of work are further explained and are illustrated.
As shown in Figure 1, current vortex sensor and induction steel disc are applied in the inner frame angle measuring system design of many frameworks photoelectric nacelle, to improve angle-measurement accuracy by the present invention.Wherein, current vortex sensor is direct current supply, and the optional+24V of voltage or ± 15V, output voltage is chosen as-2--18V or 0-5V.Induction steel disc material requires to be No. 45 steel.L in the range ability of current vortex sensor 1, output voltage and current vortex sensor and induction steel disc spacing proportional, if scale-up factor is k 1.Current vortex sensor can to slight distance high-acruracy survey (can reach micron level), so the feature little according to inner frame slewing area, the distance the caused change utilizing electric vortex sensor measuring to rotate, then obtains rotational angle according to the relation of this Distance geometry radius of gyration.
As shown in Figure 2, the azimuth axis of many frameworks gondola and pitch axis all adopt inside and outside two-layer Frame Design, so inner frame comprises orientation framework and pitching frame.
As shown in Figure 3, current vortex sensor and induction steel disc are installed on the installation frame of inner frame to be measured and this inner frame respectively.
The installation site of current vortex sensor:
As shown in Figure 4, current vortex sensor and the detail location responding to steel disc in the present invention.Current vortex sensor high order end position is A 1, induction steel disc position is B.The linear measurement range of current vortex sensor is at A 1and A 3between, string A 1a 3length is L 1.OA 2perpendicular to A 1a 3, intersection point is O '.When current vortex sensor is positioned at A 2time, its surface is just right with induction steel disc.Current vortex sensor distance perspective answers the some A of the minor increment of steel disc 3distance induction steel disc spacing is L 3(because current vortex sensor is in consistent change, so the position of distance steel disc is also in real-time change), general L 3≈ 1mm.
The range Theta that takes measurement of an angle is determined by inner frame design requirement, is generally less than ± 3 ° (or 6 °); Current vortex sensor linear measurement range L 1product attribute, generally at 6mm.The measured value of current vortex sensor is from a nonzero value, and namely measured value is 1 to 7 millimeters.
The installation site of current vortex sensor is R apart from the length in the axle center of inner frame to be measured 1, described R 1for wherein L 1for the range of current vortex sensor, θ are the required angular range measured, described R 1under meeting the prerequisite of inequality, R 1value should be as far as possible close
In the installation process of current vortex sensor and induction steel disc, concrete structural condition be considered, the size of such as pitch axis, whether with other device interference etc.R 1value is as far as possible large, because under the condition determined in current vortex sensor distance accuracy, radius is larger, and angle-measurement accuracy is higher.
When inner frame to be measured rotates relative to its installation frame, current vortex sensor changes relative to the distance of induction steel disc, and current vortex sensor exports and changes relevant voltage signal V to distance;
The voltage signal that current vortex sensor exports, by filtering and analog to digital conversion, simultaneously according to scale factor and the analog-to-digital amplification coefficient of current vortex sensor, calculates current vortex sensor and induction steel disc distance h; In the present invention, current vortex sensor is exactly the distance of current vortex sensor probe plane center point P to steel disc to the distance h of induction steel disc, calculates according to measured value wherein k 1represent the scale factor of current vortex sensor, n represents analog-to-digital figure place, and η represents analog-to-digital input voltage range.
According to the distance h of current vortex sensor and induction steel disc, the angle between the installation frame calculating inner frame to be measured and this inner frame.
According to the distance h of current vortex sensor and induction steel disc, the specific implementation of the angle beta between the installation frame calculating inner frame to be measured and this inner frame is as follows:
As shown in Figure 5, being X-axis with OB, is that initial point sets up rectangular coordinate system xOy with O.OB=R 1, straight line l represented the straight line on steel disc surface, and α is the angle of the induction straight line at steel disc place and the axle center of inner frame to be measured and steel disc line.
α = arcsin ( 0.5 L 1 + L 3 R 1 ) .
The equation of the straight line l at induction steel disc place is
y=tanα(x-R 1)。
Point P is taking round dot as the center of circle, and radius is R 1, polar angle from arrive circular arc on.The coordinate of some P is,
x = R 1 cos β y = R 1 sin β ,
Wherein, visible, the framework angle beta of actual measurement is larger than the frame corners range Theta of requirement.
So according to mathematical relation, the distance of some P to straight line l is
h = R 1 sin β - R 1 cos β tan α + R 1 tan α 1 + tan 2 α .
Wherein, R 1, α is known, h = Vη k 1 2 n , Solving equation h = R 1 sin β - R 1 cos β tan α + R 1 tan α 1 + tan 2 α , β can be calculated.
Concrete solution procedure is as follows
According to formula h = R 1 sin β - R 1 cos β tan α + R 1 tan α 1 + tan 2 α Obtain following formula:
sin β = h 1 + tan 2 α R 1 + cos β tan α - tan α
And in conjunction with sin 2β+cos 2β=1, can obtain,
(1+tan 2α)cos 2β+2atanαcosβ+a 2-1=0
Wherein, c = h 1 + tan 2 α R 1 a = c - tan α ;
Because 0≤cos β≤1, so
cos β = 1 - c 2 + 2 c tan α - c tan α + tan 2 α 1 + tan 2 α ,
Then,
β = arc cos ( 1 - c 2 + 2 c tan α - c tan α + tan 2 α 1 + tan 2 β ) .
When precise requirements is not high, because α is very little, tan α ≈ 0 can be thought, according to formula cos β = 1 - c 2 + 2 c tan α - c tan α + tan 2 α 1 + tan 2 α Can obtain,
cos 2 β + ( h R 1 ) 2 = 1
So, because β is also very little, can think
β ≈ h R 1 .
The installation site of induction steel disc and current vortex sensor can exchange, and is installed on the installation frame of inner frame to be measured and this inner frame respectively, the angle of the installation frame of inner frame to be measured and this inner frame β 1 = arccos ( 1 - c 1 2 + 2 c 1 tan α 1 - c 1 tan α 1 + tan 2 α 1 1 + tan 2 α 1 ) , Wherein α 1for the angle of the straight line at current vortex sensor place and the axle center of inner frame to be measured and current vortex sensor line;
With a specific embodiment, the course of work of the present invention is explained further below:
As shown in Figure 3 and Figure 4, O is the rotation axis of pitching frame, and the radius of clean-up of current vortex sensor is R 1.Select to get θ=6 ° here, L 1=6mm.So, select R 1for 55mm.
The minimum distance L of current vortex sensor and steel disc 3=1mm.
According to formula α = arcsin ( 0.5 L 1 + L 3 R 1 ) , Calculate α=4.17 °.
Current vortex sensor is energized, and its output signal, after a simulation low-pass filter, utilizes analog to digital converter to be converted to digital signal.If analog to digital converter input voltage range is 0-5V, change figure place into 16, then the amplification coefficient of analog to digital converter is k d=13107.The scale factor k of current vortex sensor 1=0.83V/mm.Current vortex sensor distance accuracy is 5 microns, so its angle measurement accuracy is about 0.0052 °.
The conversion value of microcomputer reads analog to digital converter is μ ∈ [0,65535], then current vortex sensor and steel disc spacing so the high pitching frame angle of accuracy requirement is according to formula
β = arc cos ( 1 - c 2 + 2 c tan α - c tan α + tan 2 α 1 + tan 2 β ) Calculate, the low pitching frame angle of accuracy requirement is according to formula calculate.
Fig. 6 gives exact value and the coarse value relation relative to ADC value, and Fig. 7 gives difference between the two.Visible, both differences are maximum reaches 0.46mrad or 0.026 °.So application person can according to the demand of degree of accuracy being selected to this two formula.
The unexposed part of the present invention is the open general knowledge in this area.

Claims (6)

1., by a method for electric vortex sensor measuring many frameworks gondola inner frame angle, it is characterized in that:
Current vortex sensor and induction steel disc are installed on the installation frame of inner frame to be measured and this inner frame respectively;
When inner frame to be measured rotates relative to its installation frame, current vortex sensor changes relative to the distance of induction steel disc, and current vortex sensor exports and changes relevant voltage signal V to distance;
The voltage signal that current vortex sensor exports, by filtering and analog to digital conversion, simultaneously calculates current vortex sensor and induction steel disc distance h according to the scale factor of current vortex sensor and analog-to-digital amplification coefficient;
According to the distance h of current vortex sensor and induction steel disc, the angle between the installation frame calculating inner frame to be measured and this inner frame.
2. the method for a kind of electric vortex sensor measuring many frameworks gondola inner frame angle according to claim 1, is characterized in that: the installation site of described current vortex sensor is R apart from the length in the axle center of inner frame to be measured 1, described R 1for wherein L 1for the range of current vortex sensor, θ are the required angular range measured, described R 1under meeting the prerequisite of inequality, R 1value should be as far as possible close
3. the method for a kind of electric vortex sensor measuring many frameworks gondola inner frame angle according to claim 2, is characterized in that: described calculating current vortex sensor and induction steel disc distance wherein, k 1represent the scale factor of current vortex sensor, n represents analog-to-digital figure place, and η represents analog-to-digital input voltage range.
4. the method for a kind of electric vortex sensor measuring many frameworks gondola inner frame angle according to claim 3, it is characterized in that: the described distance h according to current vortex sensor and induction steel disc, the specific implementation of the angle beta between the installation frame calculating inner frame to be measured and this inner frame is as follows:
(4a) the angle α of the induction straight line at steel disc place and the axle center of inner frame to be measured and steel disc line is calculated:
α = arcisn ( 0.5 L 1 + L 3 R 1 )
Wherein, L 3represent that current vortex sensor distance perspective answers the minor increment of steel disc;
(4b) the angle α and distance h that obtain in step (4a) is utilized, the angle beta between the installation frame calculating inner frame to be measured and this inner frame:
β = arccos ( 1 - c 2 + 2 c tan α - c tan α + tan 2 α 1 + tan 2 α )
Wherein, c = h 1 + tan 2 α R 1 .
5. the method for a kind of electric vortex sensor measuring many frameworks gondola inner frame angle according to claim 4, it is characterized in that: the angle beta between described inner frame to be measured and the installation frame of this inner frame, when measuring accuracy requires lower, formula of reduction can be utilized to calculate, and formula of reduction is:
6. the method for a kind of electric vortex sensor measuring many frameworks gondola inner frame angle according to claim 5, it is characterized in that: described induction steel disc and the installation site of current vortex sensor can exchange, be installed on the installation frame of inner frame to be measured and this inner frame respectively, the angle of the installation frame of inner frame to be measured and this inner frame β 1 = arccos ( 1 - c 1 2 + 2 c 1 tan α 1 - c 1 tan α 1 + tan 2 α 1 1 + tan 2 α 1 ) , Wherein α 1for the angle of the straight line at current vortex sensor place and the axle center of inner frame to be measured and current vortex sensor line; c 1 = h 1 + tan 2 α 1 R 1 .
CN201410830428.9A 2014-12-26 2014-12-26 A kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle Active CN104567653B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410830428.9A CN104567653B (en) 2014-12-26 2014-12-26 A kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410830428.9A CN104567653B (en) 2014-12-26 2014-12-26 A kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle

Publications (2)

Publication Number Publication Date
CN104567653A true CN104567653A (en) 2015-04-29
CN104567653B CN104567653B (en) 2016-06-29

Family

ID=53084283

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410830428.9A Active CN104567653B (en) 2014-12-26 2014-12-26 A kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle

Country Status (1)

Country Link
CN (1) CN104567653B (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106667610A (en) * 2015-11-09 2017-05-17 北京骇思信息科技有限公司 Electric toothbrush
CN106667609A (en) * 2015-11-09 2017-05-17 北京骇思信息科技有限公司 Electric toothbrush
CN105243364B (en) * 2015-09-24 2018-10-19 北京贯中精仪科技有限公司 Photoelectric nacelle searching method, device and system
CN109931864A (en) * 2019-03-19 2019-06-25 合肥工业大学 Spherical hinge space three-dimensional angle of revolution measurement method based on eddy current effect
CN110702038A (en) * 2019-10-15 2020-01-17 中国航空工业集团公司洛阳电光设备研究所 System for measuring platform absolute angle in pod product and data processing method

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6018704A (en) * 1983-07-12 1985-01-30 Yaskawa Electric Mfg Co Ltd Angle detecting system by resolver
CN102501979A (en) * 2011-11-10 2012-06-20 河北汉光重工有限责任公司 Airborne navigation nacelle
CN102829714A (en) * 2012-08-16 2012-12-19 中国科学院西安光学精密机械研究所 Method for realizing absolute angle measurement based on round inductosyn
CN202692936U (en) * 2012-08-15 2013-01-23 高玉琴 Rotation angle measuring device
CN104048595A (en) * 2014-06-27 2014-09-17 西安交通大学 Angle misalignment fault quantitative detection system and method for rotating machine

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6018704A (en) * 1983-07-12 1985-01-30 Yaskawa Electric Mfg Co Ltd Angle detecting system by resolver
CN102501979A (en) * 2011-11-10 2012-06-20 河北汉光重工有限责任公司 Airborne navigation nacelle
CN202692936U (en) * 2012-08-15 2013-01-23 高玉琴 Rotation angle measuring device
CN102829714A (en) * 2012-08-16 2012-12-19 中国科学院西安光学精密机械研究所 Method for realizing absolute angle measurement based on round inductosyn
CN104048595A (en) * 2014-06-27 2014-09-17 西安交通大学 Angle misalignment fault quantitative detection system and method for rotating machine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105243364B (en) * 2015-09-24 2018-10-19 北京贯中精仪科技有限公司 Photoelectric nacelle searching method, device and system
CN106667610A (en) * 2015-11-09 2017-05-17 北京骇思信息科技有限公司 Electric toothbrush
CN106667609A (en) * 2015-11-09 2017-05-17 北京骇思信息科技有限公司 Electric toothbrush
CN109931864A (en) * 2019-03-19 2019-06-25 合肥工业大学 Spherical hinge space three-dimensional angle of revolution measurement method based on eddy current effect
CN109931864B (en) * 2019-03-19 2020-08-07 合肥工业大学 Ball hinge space three-dimensional rotation angle measuring method based on eddy current effect
CN110702038A (en) * 2019-10-15 2020-01-17 中国航空工业集团公司洛阳电光设备研究所 System for measuring platform absolute angle in pod product and data processing method

Also Published As

Publication number Publication date
CN104567653B (en) 2016-06-29

Similar Documents

Publication Publication Date Title
CN104567653B (en) A kind of method of electric vortex sensor measuring many frameworks gondola inner frame angle
CN111076880B (en) Multi-point deflection measuring method of long-span bridge considering camera attitude change
CN102706361B (en) A kind of high precision many inertial navigation systems attitude accuracy assessment method
CN104990547B (en) The method and apparatus that a kind of stable fiber gyro keeps constant multiplier
CN104006787A (en) High-precision attitude determination method for spacecraft attitude motion simulation platform
CN101709975A (en) Estimation and compensation method for unbalanced moment of aerial remote sensing inertially stabilized platform
CN103234512A (en) Triaxial air bearing table high-precision attitude angle and angular velocity measuring device
CN206193235U (en) Electric power inspection is two -dimensional laser radar calibration device for robot
CN102141373A (en) Light spot center real-time detection system and detection method
CN106595638B (en) Three-axis air-bearing table attitude measuring and measurement method based on photoelectric tracking technology
ITRM20120664A1 (en) HIGH PRECISION SOLAR ELECTRONIC COMPASS.
CN109238175A (en) A kind of space plane angle measurement method based on laser tracker
CN107991691B (en) Satellite navigation positioning accuracy verification equipment and method
CN104990533A (en) Ultra-high precision attitude measuring method and device of satellite ground physical simulation system
CN103335632A (en) High-precision high-frequency response platform inclined angle measuring device and method for measuring platform inclined angle by adopting same
CN103954267A (en) Linear array CCD (Charge Coupled Device)-based secondary platform levelness measurement system and method
CN104506821A (en) Fast positioning system of ferry personnel falling into water based on digital image measurement
CN105241395B (en) For the face shape of space oversize structure and apart from high-precision measuring method
CN104535078A (en) Measuring method for flying object through photoelectric equipment based on marking points
CN103335618B (en) Inner load attitude measurement device for onboard photoelectric platform
CN103808299A (en) Sun sensor
CN105606125A (en) Test apparatus and method for inertial stabilization device
EP3783306B1 (en) Device for measuring relative heights
Sydenham Transducers in measurement and control
CN105181999A (en) High precision and continuously measuring photoelectric wind direction sensor and wind direction measuring method

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant