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GB2166920A - Measuring angular deviation - Google Patents

Measuring angular deviation Download PDF

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Publication number
GB2166920A
GB2166920A GB08527492A GB8527492A GB2166920A GB 2166920 A GB2166920 A GB 2166920A GB 08527492 A GB08527492 A GB 08527492A GB 8527492 A GB8527492 A GB 8527492A GB 2166920 A GB2166920 A GB 2166920A
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United Kingdom
Prior art keywords
target
centre
regions
ofthe
constructed
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
GB08527492A
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GB2166920B (en
GB8527492D0 (en
Inventor
Dr Bernhard F Gachter
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.)
Leica Geosystems AG
Original Assignee
Wild Heerbrugg AG
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 Wild Heerbrugg AG filed Critical Wild Heerbrugg AG
Publication of GB8527492D0 publication Critical patent/GB8527492D0/en
Publication of GB2166920A publication Critical patent/GB2166920A/en
Application granted granted Critical
Publication of GB2166920B publication Critical patent/GB2166920B/en
Expired legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/26Measuring arrangements characterised by the use of optical techniques for measuring angles or tapers; for testing the alignment of axes
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S3/00Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
    • G01S3/78Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
    • G01S3/782Systems for determining direction or deviation from predetermined direction
    • G01S3/785Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
    • G01S3/786Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically
    • G01S3/7864T.V. type tracking systems
    • G01S3/7865T.V. type tracking systems using correlation of the live video image with a stored image

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Multimedia (AREA)
  • Electromagnetism (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Optical Transform (AREA)

Abstract

The angular deviation of an object is measured using an object-related target mark constructed as an optically structured screen, and using digital photoelectric evaluation of the target image. The information values obtained are compared with a reference corresponding to the target mark. The target 1, provided with a clearly defined centre 9, is imaged onto a detection plane 10 of a receiving apparatus 3. The resulting target image is scanned with the aid of a subdivided position-sensitive, photoelectric detector 5 provided with detection regions 11 within the detection plane 10. The resulting values undergo correlation comparison 6 with values derived from the stored reference and from this is calculated the deviation of the centre of the target from the optical axis. It has proved particularly advantageous to have a mark comprising constructed as a radial pattern with circular sectors of alternately light and dark regions (7, 8. fig 4), which coverage in the common centre (9, fig 4) and in which adjacent regions subtend a random angle. <IMAGE>

Description

SPECIFICATION Measurement of angular deviation Field of Invention The invention relates to measurement of angular deviation and concerns a method and an apparatus for measuring the angular deviation of an object with the aid of target marks or targets constructed as optically structured screens.
Background to the Invention Forthe measurement of angular deviations, such as eg occur in geodesic instruments such as theodolites, levels and the like, hitherto essentially purely optical methods have been used. With the introduction of electronic means for range finding with such equipment, there is an increasing discrepency in the accuracy of the measured results as obtained on the one hand via the electronic means and on the other via purely optical means during angular measurements.
Swiss patent 638057 discloses an apparatus for determining the direction of a target by determining the position of an objectified or projected image of the target on a transmitted light screen. The target is optically structured as a reflected light screen with rotationally symmetrical, substantially radially directed, alternating light and dark divisions. The receiving apparatus essentially comprises a lens or objective directed on to the target, a transmitted light screen and behind the latter radiation detectors, together with an evaluation circu it. The transmitted light screen has the same optical structure as the reflected light screen, is rotatable about its centre of symmetry and driven by a motor. The centre ofthe transmitted light screen and the centre of the radiation detectors are aligned with the optical axis of the lens.
For determining the angular deviation ofthe target with respect to the optical axis of the lens a modulation of the signals emitted by the radiation detectors is brought about by rotating the transmitted lightscreen.
This modulation is evaluated by the evaluation circuit, which calculates the deviation and makes available corresponding values. These values are stored, displayed or supplied in some other way.
A disadvantage of this apparatus is the considerable expenditure involved on mechanical and electronic equipment, including the driveforthetransmitted light screen whilst avoiding vibrations, and the regulation ofthe rotational speed within a range which is admissibleforthe calculation. Afurther disadvantage is that the screen can only be changed with difficulty, so that it is not possible when used under practical conditions to process several targets located inthefield of vision ofthe apparatus without manual accesstothe latter. Itistherefore impossible to use the apparatus for identifying several different marked targets.
The present invention aims to provide an improved method and apparatus of the aforementioned type so asto enable the high speed measurementofthe angular deviation, whilst eliminating as far as possible reading errors, the integration ofthe method and/or apparatus into electronic range finders being desirable. The invention also aims to provide a method and apparatus with which it is possible to carry out very acurate measurements on inaccessible or hard of access objects, and with which it is possible to identify several differently marked targets.
Summary of the Invention According to one aspect ofthe invention, there is provided a method for measuring the angular position of an object with the aid of object-related targets or target marks constructed as optically structured screens by the digital photoelectric evaluation of an image ofthetarget mark and the comparison ofthe thus obtained information values with a reference mark corresponding to thetarget mark, wherein the target provided with a clearly defined centre is imaged within a receiving apparatus as a target image directly on the detection plane, serving as an image plane, of a position-sensitive photoelectric detector subdivided into detection regions, wherein the thus obtained values are compared with the reference markorwith stored values which characterisethe reference mark andwhereinfrom the comparison resultthe deviation of the centre of the target from the optical axis of the receiving apparatus is calculated.
In a further aspect the invention provides apparatus for performing the method ofthe invention, wherein a planar radiation detector provided with detection regions is arranged in fixed manner in the receiving apparatus with its optical axis, the centre thereof located on said optical axis, wherein the detection regions are connected via connecting lines to the input of a comparison computer and wherein to the latter is connected a memory means in which are stored the reference marks or characteristic values of such reference marks corresponding to the target to be surveyed.
An advantage ofthe invention is that need not require the use of mechanically moving parts, eg rotary parts. Further, the photoelectric detector may comprise a diode array, which is a particularly simple, inexpensive radiation detector. As computers already exist in such apparatus, the additional computer requirementforthe invention leads to no significant extra expenditure with respect to the present apparatus.
In embodiments using a scale-invariantconstruc- tion as the target, it is also possible to detect targets which are obliqueto the optical axis on difficulty accessable or inaccessable target objects.
It is also possible to store several reference marks in the apparatus, which makes it possible to process several targets located in the field of vision thereof, without manual intervention in the apparatus being required for changing reference marks. This leads to the possibility of a particularly simple and reliable target identification in the case of multiple measurements.
Briefdescription ofthe drawings The invention is described in greater detail hereinafter, by way of example, with reference to the accompanying drawings, in which: Figure lisa diagrammatic representation of an apparatus according to the invention; Figure 2 illustrates a first construction of a target with a centrosymmetrical pattern; Figure 3 illustrates a second construction of a target with a mosaic-like surface pattern; and Figure 4 illustrates a third construction of a target mark with a pseudostochastic radial pattern.
Detailed description ofthe drawings The arrangement illustrated in Figure 1 comprises a target or target mark 1, which is linked or associated with the object to be surveyed and which is located in the optical axis 2 of a receiving apparatus 3. Apparatus 3 comprises a lens 4 aligned on the optical axis 2, a position-sensitive radiation detector5 and computer means6towhich can be connected astoreormemory means 15.
The target 1 is constructed as a reflected light screen and is optically structured by divisions into light and dark areas 7,8, respectively. However, the target can also be constructed as a transmitted light screen without there being any need to modify the essential features ofthe method or apparatus. A predetermined point of the target 1 ,which is surrounded by light and dark areas 7,8 is defined as centre 9. Target 1 is intersected in the sighted point 14 by the optical axis 2 ofthe receiving apparatus 3. Suitable arrangements of patterns of light and dark areas, eg in the form of a radial or mosaic pattern, will be discussed below.
An image ofthe targetto be processed is stored in the store 15 as a reference markforcomparison purposes. Storage can take place by means ofthe actual optical image ofthe reference mark or by means of suitably processed characteristic values of said mark. It is also possible to store images or characteristic values of reference marks corresponding to several different targets.
Radiation detector5 is eg ofthe so-called sector type, being subdivided into several radiation-sensitive detection regions 11 which constitute the radiation sensitivesurface. The detection regions 11 are arranged regularly in a detection plane 10, eg in a circle or in matrix-like manner.
In the preferred embodiment the radiation-sensitive detection regions 11 of such a radiation detector 5 are constructed as a matrix of diodes on a semiconductor substrate, being known as a diode array. Each of these radiation-sensitive diodes is led to the outside via electrodeterminals.A base electrode is common to all the detection regions. In the preferred embodiment a ~particular point ofthe radiation-sensitive surface of the radiation detector 5 is defined as the centre 12, which is surrounded by the detection regions 11.
When selecting the dimensions ofthe lens 4, the dimensions ofthe target 1 and the radiation detector 5 must be taken into account in such a waythat an image objectified or projected by lens4 onto detection plane 10 adequately covers the radiation- sensitive surface of radiation detector 5. If the centre 9 of the target is alongside the optical axis 2, it is necessaryforthe image oftarget 1 in detection plane lOtocoverthe radiation-sensitive surface of radiation detector 5 by a minimum percentage, eg up to 20%, so as to ensure clarity in target detection and conse quently ensu re an adequate precision ofthe position determination.
Detection regions 11 are connected bylines 13to computer means 6 which, from thethus supplied signals, calculates the deviation ofthe projected centre 9 oftarget 1 in the detection plane 10 from the centre 12 ofthe radiation-sensitive surface of radiation detector 5. It is possible to derive therefrom the deviation ofthe centre 9 oftarget 1 from the sighted point l4atwhich the optical axis 2 intersects target 1.
The computer compares the optical structure of target 1 or its projected image in the detection plane 10 of radiation detector5with a pattern corresponding to the optical structure of the target and stored in computer 6 or its memory 15. The optical structure of thetargetimage is supplied to the computer by the signals ofthe plurality of detection regions 11 of radiation detector 5. At output 16 of computer6,the signals are made available for display orfor storage or furtherprocessing.Acorrelation comparison can in particular be provided as a comparison algorithm for computer 6.
The comparison performedbycomputer6for determining the angulardeviation ofthetargetorthe objectlinkedtherewith can take place in different ways. For example, the autocorrelation function ofthe stored pattern stored in store 15 may be compared with the correlation function between the pattern and the target The deviation is then calculated from the comparison result. Such correlation calculations are fundamentally known and do not have to be described in detail here. The calculation can be performed by corresponding programing of computer 6.
As a further possibility, the computer can form a cross-correlation between the stored reference pattern image andthetarget image. The sought angular deviation is then associated with the maximum value obtained, iethe empirically determined maximum of the cross-correlation function. This calculation can alsotakeplacethrough corresponding programming of computer 6.
Referring to Figure 2, the illustrated example of target 1 comprises a centrosymmetrical radial pattern oflightand dark regions. The alternately light and dark regions 7 and 8 are arranged in the form of radial sectors around centre9 and are angularly displaced with respect to one another by a clearly defined centre angle. The advantage of such an arrangement is in its scale-invariance during the correlation calculation in computer 6. This meansthatthe representation ofthe target on radiation detector Scan take place with a constant scale th roughoutthe measuring process.
In place ofthe previously described overall comparison by computer 6 in the case of such centrosymmetrical targets, according to a variantthe centre of a target can be determined by detecting the edges or boundaries between the regions of different intensity.
For example, along the radially or otherwise regularly oriented edges with respect two the centre, the edges are detected from a measurement of correspondingly arranged or selected picture or image elements. This can take place by an individual comparison of selected image points. Corresponding interpolation methods orthe algorithms necessary for the calculation are known per so and need not be described in detail.
According to another embodiment shown in Figure 3,thetarget 1 is constructed asa mosaic pattern of light and dark areas. In this case the distribution of the light and dark mosaic elements 7 or8 around the centre 9 oftarget 1 is stochastic or at least pseudos tochastic. This leads to particularly good reliability and accuracy during the cross-correlation comparison. Diverging from the representation shown, the mosaic elements can also have a different size. The evaluation of the target image in the computer takes place in the same way as described hereinbefore in connection with the target of Figure 2. The target of Figure 3 is particularly advantageous in conditions in which range information is available, because the selected pseudostochastic pattern is not scale-in- variant.
According to a further embodiment shown in Figure 4, the target 1 is constructed as a radial pattern with a stochastic or pseudostochastic radial division The aternately light and dark areas 7,8 are arranged around centre 9 as radial sectors, whose centre angle has stochastically distributed, non-regularvalues.The radial pattern according to Figure 4 is scale-invariant, likethatofFigure2,sothatwhen evaluating the measurement there is no need for any correction corresponding to the distance between the target and the receiving apparatus.
Compared with the embodiments of Figures 2 and 3, the construction ofthe target according to Figure 4 offers a further, important advantage. If the plane of target 1 is oblique instead of perpendicularto the optical axis, through a simple, perse known homothe tictransformation in the computer, the target is mathematically straightened. Through such a scale transformation in an axis passing through the centre ofthetargetimage, ina simple, butveryeffective manner, a precise angular measurement is still possible if the target is oblique or is located on poorly accessible of inaccessible objects.
According to an already mentioned advantageous construction ofthe present apparatus several reference patterns, A, B, Cetc are stored in computer 6 or memory 15 associated therewith and correspond to several alternatively usable target patterns. Through simple programmed switching in computer 6 from one reference pattern to another it is possible to process several targets located in the field of vision of receiving apparatus 3, the apparatus being in a position to clearly differentiate, ie identify different targets. The direction determination oriented on one of these targets is not disturbed by the othertargets also inthefield of vision of the receiving apparatus during the comparison with the reference mark sought from memory 15.The measurements obtained are clear and unambiguous through the association between reference and target mark performed in the computer.
Non-scale-invariant target marks, eg sighting targets subdivided in mosaic-like manner and much as in the embodiment shown in Figure 3, permitthe provision of a fine code superimposed on the basic pattern by an appropriate choice of the pattern distribution. This fine code can be additionally evaluated by the receiving apparatus and in the present case it can contain additional information concerning its relative geometrical position within the target. The fine code can eg be provided in the form of a bar code on the dark areas 8 according to Figure 3, so that these areas are also screen-patterned. On the other hand this improves the clarity for detecting thetargetfor short distances, and on the other hand for longer distances facilitates the detection by differing shades of grey caused by the fine code.

Claims (16)

1. A method for measuring the angular position of an object with the aid of object-related targets or target marks constructed as optically structured screens bythe digital photoelectric evaluation of an image ofthe target mark and the comparison of the thus obtained information values with a reference mark corresponding to the target mark, wherein the target provided with a clearly defined centre is imaged within a receiving apparatus as a target image directly on the detection plane, serving as an image plane, of a position-sensitive photoelectric detector subdivided into detection regions, wherein the thus obtained values are compared with the reference mark or with stored values which characterise the reference mark, and wherein from the comparison resultthe deviation ofthe centre of the targetfrom the optical axis of the receiving apparatus is calculated.
2. A method according to claim 1, wherein a cross-correlation comparison is performed, the maximum of the cross-correlation being determined and the determined value being used to determine the sought angular deviation of the target centre from the optical axis of the receiving apparatus.
3. A method according to claim 1 or 2, wherein in the case of several target images located in the field of vision ofthe receiving apparatus, a correlation comparison is performed with a stored supply of reference images or their characteristic values.
4. A method according to claim 1,2 or3, using centrosymmetrical targets, wherein characteristic target image contents oriented mathematically on the target centre are scanned for image points by the detector, and wherein the scan result undergoes image processing with the aid of a previously defined algorithm and is based on the comparison operations with previously stored reference values.
5. Apparatus for performing the method according to claim 1,comprising a planar radiation detector, provided with detection regions, arranged in fixed manner in the receiving apparatus, the centre of the detector being located on the optical axis of the receiving apparatus, the detection regions being connected to the input of computer means, with the computer means being connected to memory means in which are stored reference marks or characteristic values of such reference marks corresponding to the targetto be surveyed.
6. Apparatus according to claim 5, wherein the target mark is constructed as a radial pattern with circular sectors of alternating light and dark regions converging in a common centre.
7. Apparatus according to claim 6, wherein the centre angles of adjacent regions have stochastically selected differing values.
8. Apparatus according to claim 6, wherein the centre angles of adjacent regions have pseudos tochasticallyselected differing values.
9. Apparatus according to claim 5, wherein the target is constructed ass mosaic pattern with light and dark regions, which are arranged around a clearly defined centre.
10. Apparatus according to claim 9, wherein the mosaic pattern is constructed round the centre in accordance with a stochastic distribution ofthe light and dark regions.
11. Apparatus according to claim 9, wherein the mosaic pattern is constructed according to a pseudos tochastic distribution ofthe light and dark regions around the centre.
12. Apparatus according to claim 9,10 or 11, wherein at least portions ofthe regions on the target are constructed corresponding to a fine code containing additional information.
13. Apparatus according to claim 12, wherein a fine code related to the relative geometrical position within thetarget is provided on selected regions ofthe latter as additional information.
14. Apparatus according to claim 13,wherein the fine code is placed on the dark regions ofthetarget in such a way that said dark regions are interrupted by lightfine code patterns or vice versa.
15. Amethodformeasuringangulardeviation substantially as herein described with reference to the accompanying drawings.
16. Apparatusformeasuring angular deviation substantially as herein described with reference to, and as shown in, the accompanying drawings.
GB08527492A 1984-11-08 1985-11-07 Measurement of angular deviation Expired GB2166920B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH537284A CH665715A5 (en) 1984-11-08 1984-11-08 METHOD AND DEVICE FOR MEASURING THE ANGLE STORAGE OF AN OBJECT PROVIDED WITH A TARGET BRAND.

Publications (3)

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GB8527492D0 GB8527492D0 (en) 1985-12-11
GB2166920A true GB2166920A (en) 1986-05-14
GB2166920B GB2166920B (en) 1988-08-03

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JP (1) JPS61128111A (en)
CH (1) CH665715A5 (en)
DE (1) DE3538812A1 (en)
GB (1) GB2166920B (en)

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Publication number Priority date Publication date Assignee Title
FR2791431A1 (en) * 1999-03-26 2000-09-29 Sextant Avionique Optical tuning apparatus for afocal optic system includes deviator placed on optic axis, and selection of points in central zone of analysis and edge fields
WO2004023150A1 (en) * 2002-09-03 2004-03-18 Loughborough University Enterprises Limited Marking of objects for speed and spin measurements
WO2006060715A3 (en) * 2004-12-03 2006-08-10 Honeywell Int Inc Absolute position determination of an object using pattern recognition
US7274439B2 (en) 2004-09-10 2007-09-25 Honeywell International Inc. Precise, no-contact, position sensing using imaging
US7289902B2 (en) 2004-09-10 2007-10-30 Honeywell International Inc. Three dimensional balance assembly
US7340344B2 (en) 2004-09-10 2008-03-04 Honeywell International Inc. Spherical position monitoring system
US7366613B2 (en) 2004-09-10 2008-04-29 Honeywell International Inc. RF wireless communication for deeply embedded aerospace systems
US7425097B1 (en) 2007-07-17 2008-09-16 Honeywell International Inc. Inertial measurement unit with wireless power transfer gap control
US7458264B2 (en) 2004-09-10 2008-12-02 Honeywell International Inc. Generalized inertial measurement error reduction through multiple axis rotation during flight
US7617070B2 (en) 2004-09-10 2009-11-10 Honeywell International Inc. Absolute position determination of an object using pattern recognition
US7647176B2 (en) 2007-01-11 2010-01-12 Honeywell International Inc. Method and system for wireless power transfers through multiple ports
US7671607B2 (en) 2007-09-06 2010-03-02 Honeywell International Inc. System and method for measuring air bearing gap distance
US7698064B2 (en) 2004-09-10 2010-04-13 Honeywell International Inc. Gas supported inertial sensor system and method
US7762133B2 (en) 2007-07-17 2010-07-27 Honeywell International Inc. Inertial measurement unit with gas plenums
CN104677598A (en) * 2015-01-28 2015-06-03 中国科学院光电研究院 Novel artificial target for optical payload performance evaluation, and manufacturing method thereof

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DE19621195C1 (en) 1996-05-25 1997-08-21 Leica Ag Object direction measuring method
DE19922321C2 (en) * 1999-05-14 2002-07-18 Zsp Geodaetische Sys Gmbh Method and arrangement for performing geodetic measurements using a video tachymeter
DE102005032871A1 (en) * 2005-07-14 2007-01-25 Leopold Kostal Gmbh & Co. Kg Method for determining the absolute angular position of the steering wheel of a motor vehicle
CN104501745B (en) * 2015-01-19 2017-12-12 中国人民解放军国防科学技术大学 A kind of quick determination method and device of photo electric imaging system optical axis deviation
KR102313177B1 (en) * 2020-08-07 2021-10-18 주식회사 액트로 System and method to check the rotation angle of the prism included in the camera module

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GB2007455A (en) * 1977-11-02 1979-05-16 Hughes Aircraft Co Video correleation tracker
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Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2791431A1 (en) * 1999-03-26 2000-09-29 Sextant Avionique Optical tuning apparatus for afocal optic system includes deviator placed on optic axis, and selection of points in central zone of analysis and edge fields
WO2004023150A1 (en) * 2002-09-03 2004-03-18 Loughborough University Enterprises Limited Marking of objects for speed and spin measurements
US7698064B2 (en) 2004-09-10 2010-04-13 Honeywell International Inc. Gas supported inertial sensor system and method
US7274439B2 (en) 2004-09-10 2007-09-25 Honeywell International Inc. Precise, no-contact, position sensing using imaging
US7289902B2 (en) 2004-09-10 2007-10-30 Honeywell International Inc. Three dimensional balance assembly
US7295947B2 (en) 2004-09-10 2007-11-13 Honeywell International Inc. Absolute position determination of an object using pattern recognition
US7340344B2 (en) 2004-09-10 2008-03-04 Honeywell International Inc. Spherical position monitoring system
US7366613B2 (en) 2004-09-10 2008-04-29 Honeywell International Inc. RF wireless communication for deeply embedded aerospace systems
US7458264B2 (en) 2004-09-10 2008-12-02 Honeywell International Inc. Generalized inertial measurement error reduction through multiple axis rotation during flight
US7617070B2 (en) 2004-09-10 2009-11-10 Honeywell International Inc. Absolute position determination of an object using pattern recognition
WO2006060715A3 (en) * 2004-12-03 2006-08-10 Honeywell Int Inc Absolute position determination of an object using pattern recognition
US7647176B2 (en) 2007-01-11 2010-01-12 Honeywell International Inc. Method and system for wireless power transfers through multiple ports
US7425097B1 (en) 2007-07-17 2008-09-16 Honeywell International Inc. Inertial measurement unit with wireless power transfer gap control
US7762133B2 (en) 2007-07-17 2010-07-27 Honeywell International Inc. Inertial measurement unit with gas plenums
US7671607B2 (en) 2007-09-06 2010-03-02 Honeywell International Inc. System and method for measuring air bearing gap distance
CN104677598A (en) * 2015-01-28 2015-06-03 中国科学院光电研究院 Novel artificial target for optical payload performance evaluation, and manufacturing method thereof

Also Published As

Publication number Publication date
GB2166920B (en) 1988-08-03
CH665715A5 (en) 1988-05-31
DE3538812A1 (en) 1986-05-15
JPS61128111A (en) 1986-06-16
GB8527492D0 (en) 1985-12-11

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