Remote attitude sensor using single camera and spiral patterns

• US 4,652,917 A
• Filed: 08/10/1984
• Issued: 03/24/1987
• Est. Priority Date: 10/28/1981
• Status: Expired due to Term

• Current Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Original Assignee: Honeywell Incorporated (Honeywell International Inc.)
• Inventors: Miller, John W.
• Primary Examiner(s): NOT, DEFINED
• Assistant Examiner(s): Coles, Edward L.
• Application Number:
  US06/639,610
• Time in Patent Office: 956 Days
• Field of Search: 358/107, 358/108, 356/1, 356/3, 356/4, 356/27, 356/28, 356/21, 356/22, 356/152, 364/516, 364/562, 364/559
• US Class Current: 348/135
• CPC Class Codes: G01B 11/16 for measuring the deformation in a solid, e.g. optical strain gauge
• CPC Class Codes: G01S 17/875 for determining attitude
• CPC Class Codes: G01S 5/163 Determination of attitude using inertial means G01C9/00; control of attitude G05D1/49

Abstract

A system for monitoring the attitude of an object with respect to a fixed based without any material connection to the object, comprising imaging apparatus mounted on the base so that a surface of the object is in the field of view, targets on the surface of such spaced sites, remote from the imaging apparatus that the apparatus images the targets in relative positions determined by the locations of the sites, and computing apparatus determining from changes in the relative positions of the images the causative changes in the attitude of the object with respect to the base.

Claims

1. An apparatus for monitoring the alignment of an aircraft wing relative to a substantially rigid fuselage of said aircraft comprising:

at least first, second, and third target spots fixed in relation to said wing and defining a target plane, said target spots having median points thereof which form verticies of a triangle, said median point of said first spot defining an orgin of a co-ordinate system on said target plane;

imaging means rigidly mounted on said fuselage with a field of view including said target spots, said imaging means including an imaging lens and a two dimmensional image plane for obtaing first, second, and third spot images thereon corresponding to said target spots projected on said image plane through said imaging lens;

first means coupled to said imaging means for determining coordinates of median points of said image spots on said image plane; and

second means, responsive to signals representative of (i) said coordinates of said median points of said image spots, (ii) distances between said median points of each of said target spots, (iii) the distance between said lens and said image plane, and (iv) the distance between said lens and each of said target spots, for determining the orientation of said target plane relative to said image plane thereby providing an indication of the orientation of said wing relative to said fuselage.

2. The apparatus of claim 1 wherein said triangle is a right triangle.

3. The apparatus of claim 1 wherein:

said image plane includes a two-dimensional array of light sensitive sensors each having a known coordinate, wherein said array is defined by a fixed number of horizontal rows and vertical columns of said sensors, and wherein each of said sensors has an outout indicative of the light impinging thereon; and

said first means includes,

means for defining a tracking gate having first and second horiziontal and vertical halves, said tracking gate defining an area of an integral number of said sensors and sufficiently larger than said image spots, said tracking gate having a mid-point coordinate related to the position of said tracking gate in relation to said image plane,

means for separately summing each of said sensor outputs within each of said first and second halves of said tracking gate,

means for determining the difference between said sensor output sums of said first and second horizontal halves and the difference between said sensor output sums of said first and second vertical halves,

means for repositioning said tracking gate in response to said differences so as to optimally center said image spot within said tracking gate,

means for determining the greatest sum of said sensor outputs in a row and the greatest sum of said sensor outputs in a column within said tracking gate and about the geometrical middle defining said halves, and

computational means responsive to (i) the position of said tracking gate mid-point coordinate, and (ii) said greatest sums of said row and column for determining coordinates of the median point of said image spots on said image plane.

4. An apparatus for determining the coordinates of a median point of a target image on an image plane defined by a two-dimensional array of light sensitive sensors each having a known coordinate, wherein said two-dimensional array is defined by a fixed number of horizontal rows and vertical columns of said sensors, and wherein each of said sensors has an output indicative of the light impinging thereon, the apparatus comprising:

means for defining a tracking gate having first and second horizontal and vertical halves, said tracking gate defining an area of an integral number of said sensors and sufficiently larger than said target image, said tracking gate having a mid-point coordinate related to the position of said tracking gate in relation to said image plane;

means for separately summing each of said sensor outputs within each of said first and second halves of said tracking gate;

means for determining the difference between said sensor output sums of said first and second horizontal halves and the difference between said sensor output sums of said first and second vertical halves;

means for repositioning said tracking gate in response to said differences so as to optimally center said target image within said tracking gate;

means for determining the greater sum of said sensor outputs in a row and the greatest sum of said sensor outputs in a column within said tracking gate and about the geometrical middle defining said halves; and

computational means responsive to (i) the position of said tracking gate mid-point coordinate, and (ii) said greatest sums of said row and column for determining coordinates of the median point of said target image on said image plane.

5. The apparatus of claim 4 further comprising:

means for determining a ratio of the difference between said horizontal halves and said greatest horizontal row sum;

means for determining a ratio of the difference between said vertical halves and said greatest vertical column sum; and

said computational means including means responsive to said ratios for determing said target image median point.

6. The apparatus of claim 4 wherein said image plane is a charge couple device.

7. An apparatus for monitoring the orientation of a first object relative to a second object comprising:

at least first, second, and third target spots fixed in relation to said first object and defining a target plane, said target spots having median points thereof which form verticies of a triangle, said median point of said first spot defining an orgin of a coordinate system on said target plane;

imaging means rigidly mounted on said second object with a field of view including said target spots, said imaging means including an imaging lens and a two dimmensional image plane for obtaing first, second, and third spot images thereon corresponding to said target spots projected on said image plane through said imaging lens, said image plane including a two-dimensional array of light sensitive sensors each having a known coordinate, wherein said array is defined by a fixed number of horizontal rows and vertical columns of said sensors, and wherein each of said sensors has an outout indicative of the light impinging thereon;

first means coupled to said imaging means for determining coordinates of median points of said image spots on said image plane, said first means including,

means for defining a tracking gate having first and second horizontal and vertical halves, said tracking gate defining an area of an integral number of said sensors and sufficiently larger than said image spots, said tracking gate having a mid-point coordinate related to the position of said tracking gate in relation to said image plane,

means for separately summing each of said sensor outputs within each of said first and second halves of said tracking gate,

means for determining the difference between said sensor output sums of said first and second horizontal halves and the difference between said sensor output sums of said first and second vertical halves,

means for repositioning said tracking gate in response to said differences so as to optimally center said image spot within said tracking gate,

means for determining the greatest sum of said sensor outputs in a row and the greatest sum of said sensor outputs in a column within said tracking gate and about the geometrical middle defining said halves, and

computational means responsive to (i) the position of said tracking gate mid-point coordinate, and (ii) said greatest sums of said row and column for determining coordinates of the median point of said image spots on said image plane; and

second means responsive to changes in said median point coordinates of said image spots for determining causitive changes in the spatial relation between said first and second objects, said second means being responsive to signals representative of (i) said coordinates of said median points of said image spots, (ii) distances between said median points of each of said target spots, (iii) the distance between said lens and said image plane, and (iv) the distance between said lens and each of said target spots, for determimng the orientation of said target plane relative to said image plane thereby providing an indication of the orientation of said first object relative to said second object.