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GB2116000A - Guidance system - Google Patents

Guidance system Download PDF

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Publication number
GB2116000A
GB2116000A GB08206113A GB8206113A GB2116000A GB 2116000 A GB2116000 A GB 2116000A GB 08206113 A GB08206113 A GB 08206113A GB 8206113 A GB8206113 A GB 8206113A GB 2116000 A GB2116000 A GB 2116000A
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GB
United Kingdom
Prior art keywords
reference locations
path
view
field
predetermined location
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
GB08206113A
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GB2116000B (en
Inventor
George Brown
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.)
Allard Way Holdings Ltd
Original Assignee
Elliott Brothers London Ltd
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 Elliott Brothers London Ltd filed Critical Elliott Brothers London Ltd
Priority to GB08206113A priority Critical patent/GB2116000B/en
Publication of GB2116000A publication Critical patent/GB2116000A/en
Application granted granted Critical
Publication of GB2116000B publication Critical patent/GB2116000B/en
Expired legal-status Critical Current

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Classifications

    • 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
    • G01S5/00Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/16Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using electromagnetic waves other than radio waves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41WEAPONS
    • F41GWEAPON SIGHTS; AIMING
    • F41G7/00Direction control systems for self-propelled missiles
    • F41G7/34Direction control systems for self-propelled missiles based on predetermined target position data
    • F41G7/343Direction control systems for self-propelled missiles based on predetermined target position data comparing observed and stored data of target position or of distinctive marks along the path towards the target
    • 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
    • G01S11/00Systems for determining distance or velocity not using reflection or reradiation
    • G01S11/12Systems for determining distance or velocity not using reflection or reradiation using electromagnetic waves other than radio waves

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Navigation (AREA)

Abstract

A guidance system enables a moving body (1) to be guided to a predetermined location by allowing the body (1) to view its surroundings and to compare the viewed scene (8) with a reference pattern (e.g. 24) stored on the body. A number of individual reference patterns (24, 25, 26, 27, 28, 40 etc) are stored, and each reference pattern corresponds to an area of the surroundings (e.g. 24) which is very much smaller than the field of view (8) and thus the body identifies its position by correlating its field of view (8) with one of the reference patterns (e.g. 24). To enable the body (1) to identify its position (30) even if it deviates from an expected path (31), a number of reference patterns (e.g. 24, 25, 27, 28) are laterally displaced from the expected path (31). The extent of the lateral displacements reduces with decreasing distance from a predetermined location (40) to which the body (1) is to be guided. <IMAGE>

Description

SPECIFICATION Improvements in or relating to guidance systems This invention relates to guidance systems and is particularly concerned with systems in which a moving body is to be guided to a predetermined location. One method of enabling a body to determine its position is by allowing it to view its surroundings and to compare its field of view with a reference pattern. The process of identifying the viewed scene with a reference pattern is often termed correlation. In principle, correlation, whether it is of a one or two dimensional nature, involves searching for a particular signal or data pattern within a temporal or spatial window in another signal or data pattern.In the present invention, the signals or data patterns represent two dimensional images and thus one image is being searched for within another image, i.e. two images are of different sizes, one being a sub-setofthe other.
This aspect of correlation is sometimes termed "scene imaging by area correlation" and it can be used to bring a moving body to a predetermined location and to cause it to follow a predetermined path. It is merely necessary for the body to view its surroundings as it moves, and to compare the viewed scene with reference data relating to localised reference areas along its path. As the viewed scene is periodically correlated with the localised reference areas, the moving body can determine whether it is on the required path or whether it diverges from it, and in the latter case correction can be applied.
It is customary for the reference areas to be very much larger than the field of view so that the guidance system has the task of searching through a relatively large reference area to determine whether any portion of it correlates with its current field of view. A relatively large area is usually used since one can fairly be certain that it will contain a large number of well distributed prominent visual features of a distinctive nature, and furthermore, such an arrangement is able to tolerate relatively large positional errors associated with the movement of the body. Thus even if the body is laterally displaced by a significant extent from the required path, its position can still be determined providing that its field of view is within the boundaries of the relatively large reference area.
However, such an arrangement is very difficult to implement into a practical system, and moreover if the positional error should be so large that the optical field of view does not fall within the single reference area, guidance of the body is not possible.
The present invention seeks to provide an improved guidance system.
According to this invention a guidance system for guiding, to a predetermined location, a moving body which has means for viewing its surroundings and for correlating therewith reference locations each having an effective area much smallerthan the field of view of its surrounding, utilises a plurality of reference locations which are positioned generally along an expected approach path, with at least some of the reference locations being laterally displaced from said path, and the extent of the lateral displacements reducing with decreasing distance from said predetermined location.
Although it is likely that some of the reference locations will lie on the expected approach path, this is not essential and in practice the actual positions of the reference locations will be largely dictated by the occurrence of distinctive visual features. The means which the body has for viewing its surroundings can take many forms; it may comprise a conventional television camera operating in the visible part of the spectrum, or it may rely on infra-red detectors, or use laser beam scanners.
The kind of viewing means will be chosen in dependence on the nature of the moving body and its surroundings. For example, the moving body may be an aircraft or the like, in which case the terrain over which it flies represents its surroundings. However, the moving body could be the manipulator arm of a robot used in a manufacturing process, in which case the work piece itself constitutes part of the surroundings.
It is clearly necessary to know in advance the predetermined location and the expected approach path so that suitable reference locations can be chosen, and be encoded in a form which permits their correlation with the viewing means. If the surroundings are constituted by terrain, the reference locations take the form of localised visual features of a distinctive nature, and are chosen such that there is only a single such visual feature within the field of the view of the viewing means at any one time. The localised visual features can be extracted from photographs of the terrain or from suitable maps, whichever is the more convenient. In the case of the manipulator arm, mentioned previously, distinctive visual features can be artificially inserted into the surroundings at convenient positions so as to ease the task of correlation.
Generally the reference locations will be held in the form of data patterns, and will be stored so as to be rapidly compared with the field of view of the scanning means. The data pattern is preferably in the form of binary digits, since in this form it can be used by a digital correlator, but it is, of course, necessary for the viewed scene to be converted to a compatible form of binary digits, prior to correlation.
The predetermined location may be the final destination of the moving body, or it may instead be merely a position on a predetermined and unique path along which the body is subsequently required to move. In this latter case, the plurality of laterally displaced reference locations serve to acquire, or gather, the moving body and allow for the possibility that the body may not approach from the expected direction.
The invention is further described by way of example with reference to the accompanying drawings in which, Figures 7 and 2 are explanatory diagrams, and Figure 3 shows, in diagrammatic form, a guidance system in accordance with this invention.
Referring to Figure 1, there are shown therein diagrams which enable the concept of the present invention to be compared with a previously known system. The conventional correlation system is represented in the left hand side of the Figure at A, and a moving body 1 moving in direction 2 is assumed to carry a downward looking television camera 3, which views the ground 4, which constitutes its surroundings, as it passes over it. The field of view 5 of the television camera 3 is determined by the viewing angle a which is chosen so as to achieve the best possible optical resolution in relation to the distance between the camera 3 and the ground 4.
The reference area 6 is very much larger than the field of view 5 and represents an area which is stored at the body 1, in the form of digital bindary data. The body 1 also includes a correlator which compares the viewed scene 5 with the reference data 6 until it finds a sufficiently good match. When a good match is found, it is assumed that the position of the field of view 5 within the larger reference area 6 has been precisely determined. If the linear dimension of the field of view 5 is 0 and the linear dimension of the reference area 6 is P and that, by way of example, P = 40, the the maximum distance by which the reference area 5 can depart from a predetermined path 7 is given in general by (P - Q)/2 and in this particular example by 30/2.
By way of comparison the principle of the system in accordance with the invention is illustrated in the right hand side of Figure 1, at B, where the optical system is assumed to be identical, i.e. the body 1 carries a television camera 3 having an angle field of view a and it moves in the direction 2. The field of view 8 of the television camera still has a linear dimension Q, but the size of the reference area 9 stored within the body 1 has a very small linear dimension P, Assuming that now P = Q/4 then the maximum permissible deviation of the body 1 from the path 7 is given by 3(1/8 if the position of the body 1 is to be found by correlation with the reference area 9. Thus the tolerance of the system to lateral drift or displacement is very much less than is the case represented by A in Figure 1.However, it possesses the advantage that the correlation process is very much easier to accomplish in that the incoming television video signal can be compared relatively easily with the very small quantity of reference data which characterises area 9. Fourth ermore, the actual location of the reference area 9 can be chosen so that it encompasses just one very distinctive visual feature. This is in contrast with the previous system as exemplified by A where the incoming video information from the camera 3 has to be compared with an extremely large data base as represented by the area 6 and which may contain only few distinctive features widely spaced apart.
Thus the present invention reduces drammatically the amount of data which has to be stored and handled, thereby allowing the correlation to be accomplished in a realistically short period of time, i.e. the position of the body 1 can be determined before it has moved very far to a different position.
Thus corrective action to bring the body on to a required path can be taken much more rapidly and with greater certainty of accuracy.
Figure 2 illustrates a multi-channel correlation system which enables the capture distance of the body to be made very great, in principle as great as is necessary without unrealistically increasing the amount of reference data which has to be carried by the body. It will be seen that the multi-channel system consists of a number of separate stages which progressively direct the moving body on to the predetermined path. This aspect is of considerable practical importance since initially the position of the body 1 may be unknown, and can vary randomly between wide limits.The initial capture stage 20 has a width 21, but requires only five small reference areas 24, 25, 26, 27, 28, the detaiis of which can easily be stored on the body 1 * Thus the capture width can be made as large as necessary without unrealistically increasing the data storage requirements or imposing excessive demands on the correlator process. This aspect is in contrast to the system A represented in Figure 1, where the dimension P of reference area 6 (which represents the data storage requirement) would have to be increased to an unacceptable level.
The actual path 30 of the body 1 is indicated on Figure 2, and it is displaced from the expected path 31 leading to a predetermined location. The purpose of the system is to guide the moving body onto the path 31 (or sufficiently close to it so as to be encompassed within the field of view) by the time it reaches the location 32, so that thereafter it can be made to adhere sufficiently closely to the required path'33 by means of single, subsequent, reference areas 40, (only one of which is shown) positioned at suitable distances along the path 31.
When the actual position of the body 1 has been determined at the first capture stage 20, it is caused to change direction at point 35 and steered towards the path 31.
The second stage 34, redirects the body 1 onto the correct path, but requires only three reference areas.
In practice, if the body 1 is moving very rapidly, further stages may be needed, before the body 1 can be brought sufficiently close to the path 31.
Figure 3 shows in block diagrammatic form the way in which the correlation system is implemented.
The camera 3 with its field of view of the terrain over which the body is passing generates an analogue video signal in conventional manner. This analogue signal is passed via a digital-to-analogue converter 50, which generates a digital signal representing the viewed scene, to a pre-processor 51 which converts the digital signal to a two level or binary signal, i.e.
the incoming digital data which represents the greyscale content of the video signal is converted to one representing a two tone signal (e.g. black and white) from which intermediate grey tones have been removed. The digital data then passes from the preprocessor 51 and is applied to a binary correlator 52. The video information relates to the relatively large area 8 of the field of view of the camera 3 and the purpose of the binary correlator 52 isto compare theKincoming digital data with relatively small reference areas held in active data stores 54 which can be readily and rapidly accessed. Binary correlators are, in themselves, known devices, and TRW devices such as type TDC 1004 or 1023 can be used.
The number of active data stores corresponds to the maximum number of individual reference areas of any given correlation stage shown in Figure 2.
The data relating to the individual reference areas shown in Figure 2 (there are ten such areas) is initially held in a large store 58, and as correlation stage 20 is approached, the data relating to reference areas 24 to 28 is read out of store 58 and loaded into the respective active stores 24, which being small can be designed so that they can be very rapidly accessed. Each reference area in a respective one of stores 54 is accessed sequentially by the binary correlator 52, typically on a line by line basis, assuming that all five reference areas occur at about the same distance along the expected approach path 31.
If the field of view 8 of the camera 3 encompasses one of the reference areas 24 - 28 stored within the group of stores 54, a positive correlation is found by the acquisition block 55. The position of the body 1 at the instant the appropriate field of view was viewed is compared with the position of the reference area with which correlation has been found, and an appropriate instruction is provided to the guidance block 56, so as to steer the body towards the required predetermined path 31.
As the next correlation stage 34 is approached the group of stores 54 is re-loaded from store 58 with the three references required, as shown in Figure 2. The correlation process is repeated and after a successful correlation has been achieved, the single reference area corresponding to capture stage 32 is loaded into one store of 54. The process then continues using the single reference area 40, and subsequent single reference areas (not shown) positioned at intervals along the path 31.
In Figure 2, the body 1 is shown approaching the capture stage 20 at the maximum permissible distance from the predetermined path 31 - its approach path is off-set from the predetermined path 31 by an amount such that the field of view 8 of the camera just includes the reference area 24 so that the body 1 can determine its own position. The additional areas of fields of view are indicated on this drawing, so that it can be seen that the lateral spacings of the adjacent reference areas 24 to 28 are such that each field of view includes at least one, and sometimes two, reference areas.
It is assumed that the actual path 30 of the body is sufficiently close to the required path 31 at reference stage 32 because the field of view 8 of the camera includes the single reference area which is actually on the path 31, even though the distance between the two paths is significant. This degree of accuracy is sufficient because the body 1 continues to move past stages 32 and 40 to subsequent stages (not shown), and great precision is required only at the final stage, i.e. at the ultimate destination.
Although of general application, the invention is particularly suitable for the navigation of an aircraft or missile. Conventional inertial navigation systems are liable to drift, which although small, may be significant if allowed to develop uncorrected for a long period of time. This can happen if the aircraft is flying over featureless terrain, e.g. sea or desert, and in the former case the capture stage 20 shown in Figure 2 would typically represent a strip of land lying along the coastline. Thus an aircraft making a landfall at an unknown location can quickly orientate itself and be guided to its eventual destination. Once the aircraft has been successfully guided onto its required path (e.g. path 31 on Figure 2), the subsequent reference areas can be spaced apart by relatively long distances since they are needed only to enable the conventional inertial navigation system to be updated before its drift becomes too large.

Claims (6)

1. A guidance system for guiding, to a predetermined location, a moving body which has means for viewing its surroundings and for correlating therewith reference locations each having an effective area much smaller than the field of view of its surrounding in which a plurality of reference locations positioned generally along an expected approach path, with at least some of the reference locations being laterally displaced from said path, and the extent of the lateral displacements reducing with decreasing distance from said predetermined location.
2. A system as claimed in claim 1 and wherein the plurality of reference locations are arranged in groups which are relatively widely spaced apart along said expected approach path, with the overall lateral displacements of reference locations within given groups progressively reducing in the direction towards said predetermined location.
3. A system as claimed in claim 1 and wherein, in each group containing a plurality of reference locations, at least one reference location lies close to or includes part of said expected approach path.
4. A system as claimed in claim 2 or 3 and wherein, as said moving body approaches a particular group of reference locations, data representative of them is compared with said field of view until correlation therewith is obtained, and wherein the direction of said moving body is modified in dependence on the result of said correlation so as to direct it towards the next group in a direction converging with said expected approach path.
5. A system as claimed in claim 2,3 or 4 and wherein, in each group containing a plurality of reference locations, the individual reference locations are displaced from each other in the direction of the expected approach path by amounts which are small as compared with maximum lateral displacement within that group.
6. A guidance system substantially as illustrated in and described with reference to Figures 2 and 3 of the accompanying drawings.
GB08206113A 1982-03-02 1982-03-02 Guidance system Expired GB2116000B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08206113A GB2116000B (en) 1982-03-02 1982-03-02 Guidance system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08206113A GB2116000B (en) 1982-03-02 1982-03-02 Guidance system

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GB2116000A true GB2116000A (en) 1983-09-14
GB2116000B GB2116000B (en) 1985-05-01

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2570195A1 (en) * 1984-09-07 1986-03-14 Messerschmitt Boelkow Blohm OPTOELECTRONIC TARGET SEARCH APPARATUS FOR ENTRY AND AUTOMATIC DETERMINATION OF THE GOAL ON BOARD CARRIER VEHICLES
GB2237951A (en) * 1989-11-08 1991-05-15 Smiths Industries Plc Navigation systems using passive imaging sensors
GB2258545A (en) * 1983-07-15 1993-02-10 Marconi Avionics Correlation processors
GB2258575A (en) * 1984-06-29 1993-02-10 British Aerospace Re-entry vehicle guidance system
GB2315124A (en) * 1996-07-09 1998-01-21 Gen Electric Real time tracking of camera pose
GB2320555A (en) * 1987-05-13 1998-06-24 Manfred Kusters Missile homing method
DE10139846C1 (en) * 2001-08-14 2003-02-06 Daimler Chrysler Ag Method for estimating positions and locations uses alignment of image data for a camera of model structures in order to increase long-duration stability and autonomics of aerodynamic vehicles/missiles.
EP1158309A3 (en) * 2000-05-26 2005-02-09 Honda Giken Kogyo Kabushiki Kaisha Method and Apparatus for position detection

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2258545B (en) * 1983-07-15 1993-07-21 Marconi Avionics Improvements in or relating to correlation processors
GB2258545A (en) * 1983-07-15 1993-02-10 Marconi Avionics Correlation processors
GB2258575A (en) * 1984-06-29 1993-02-10 British Aerospace Re-entry vehicle guidance system
GB2258575B (en) * 1984-06-29 1993-07-14 British Aerospace Guidance system and method
GB2165714A (en) * 1984-09-07 1986-04-16 Messerschmitt Boelkow Blohm Electro-optical aiming device
FR2570195A1 (en) * 1984-09-07 1986-03-14 Messerschmitt Boelkow Blohm OPTOELECTRONIC TARGET SEARCH APPARATUS FOR ENTRY AND AUTOMATIC DETERMINATION OF THE GOAL ON BOARD CARRIER VEHICLES
GB2320555B (en) * 1987-05-13 1998-09-23 Kusters Manfred Homing Method
GB2320555A (en) * 1987-05-13 1998-06-24 Manfred Kusters Missile homing method
US5857644A (en) * 1987-05-13 1999-01-12 Kuesters; Manfred Homing process
EP0427431A3 (en) * 1989-11-08 1992-11-25 Smiths Industries Public Limited Company Navigation systems
US5072396A (en) * 1989-11-08 1991-12-10 Smiths Industries Public Limited Company Navigation systems
GB2237951B (en) * 1989-11-08 1994-04-27 Smiths Industries Plc Navigation systems
GB2237951A (en) * 1989-11-08 1991-05-15 Smiths Industries Plc Navigation systems using passive imaging sensors
GB2315124A (en) * 1996-07-09 1998-01-21 Gen Electric Real time tracking of camera pose
US5850469A (en) * 1996-07-09 1998-12-15 General Electric Company Real time tracking of camera pose
EP1158309A3 (en) * 2000-05-26 2005-02-09 Honda Giken Kogyo Kabushiki Kaisha Method and Apparatus for position detection
US7239339B2 (en) 2000-05-26 2007-07-03 Honda Giken Kogyo Kabushiki Kaisha Position detection apparatus, position detection method and position detection program
DE10139846C1 (en) * 2001-08-14 2003-02-06 Daimler Chrysler Ag Method for estimating positions and locations uses alignment of image data for a camera of model structures in order to increase long-duration stability and autonomics of aerodynamic vehicles/missiles.

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Publication number Publication date
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PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930302