US4160267A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Switching method for measuring two neighboring flying targets or objects in succession
Assignee: Rheinmetall Air Defence AG
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Filing: 1978-05-08
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Granted: 1979-07-03
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Expires: 1998-05-08
Abstract
Abstract A switching method for measuring or tracking two neighboring flying targets in succession by means of a measuring installation having a television system. A regulation system receives course signals, which correspond to the deviation of the image of a flying target or object from the image center, and aligns the line of sight of the television camera at the flying target. An electronic window limits the formation of the deviation signals to the contribution of the image point of the flying target located in the window. During measurement of the first flying target by means of first deviation signals and a first window there is produced about the image center a second window and second deviation signals which are delimited by the second window. The first deviation signals are added, by actuating a control handle or stick to additional signals, in order to shift the line of sight and thus bring the image of the second flying target into the image center. Thereafter the regulation system is switched into operative relationship with a control by the second deviation signals. The invention is used to eliminate the effects of alignment errors and transient phenomena upon switching the measurement from one flying target to another flying target.
Inventors
- 👤 Walter Eicher
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 08:24
CPC Classifications
G; G01; G01S; G01S3/00; G01S3/78; G01S3/782; G01S3/785; G01S3/786; G01S3/7864
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
376 words
A switching method for measuring two neighboring flying targets in succession by means of a measuring installation, comprising the steps of: providing a measuring installation having an electronic observation system with image sensor and image device, a regulation system for automatically aligning the image sensor at a flying target to be measured and containing at least one first image evaluation system where there are formed from signals of the observation system a first pair of first deviation signals, one of the deviation signals constituting a measure of the momentary angular deviation in azimuth and the other deviation signal constituting a measure of the momentary angular deviation in elevation between the direction of a first flying target and the line of sight of the image sensor and delivered to the regulation system as an actual value; generating at the observation system an electronic window; framing the trace of the line of sight by means of the electronic window at the image device; limiting the processing of the signals of the observation system in the image evaluation system to such signals which correspond to an image point located at the image device within the electronic window; forming in the observation system during the automatic aligning of the image sensor at the first flying target by means of the first image evaluation system a second electronic window; positioning the second electronic window at the image device by means of a manually actuatable control means as a frame about the image of a second flying target; producing in a second image evaluation system a second pair of second deviation signals; said second pair of second deviation signals comprising such signals of the observation system which correspond to an image point located at the image device within the second electronic window; one of the second signals constituting a measure for the momentary angular deviation in azimuth and the other of said signals a measure of the momentary angular deviation in elevation between the direction of the second flying target and said line of sight; and after positioning the second electronic window at the image of the second flying target switching the actual value of the regulation system from the first pair of deviation signals to the second pair of deviation signals.
Claim 2
Dependent Claim
376 words
A switching method for measuring two neighboring flying targets in succession by means of a measuring installation, comprising the steps of: providing a measuring installation having an electronic observation system with image sensor and image device, a regulation system for automatically aligning the image sensor at a flying target to be measured and containing at least one first image evaluation system where there are formed from signals of the observation system a first pair of first deviation signals, one of the deviation signals constituting a measure of the momentary angular deviation in azimuth and the other deviation signal constituting a measure of the momentary angular deviation in elevation between the direction of a first flying target and the line of sight of the image sensor and delivered to the regulation system as an actual value; generating at the observation system an electronic window; framing the trace of the line of sight by means of the electronic window at the image device; limiting the processing of the signals of the observation system in the image evaluation system to such signals which correspond to an image point located at the image device within the electronic window; forming in the observation system during the automatic aligning of the image sensor at the first flying target by means of the first image evaluation system a second electronic window; positioning the second electronic window at the image device by means of a manually actuatable control means as a frame about the image of a second flying target; producing in a second image evaluation system a second pair of second deviation signals; said second pair of second deviation signals comprising such signals of the observation system which correspond to an image point located at the image device within the second electronic window; one of the second signals constituting a measure for the momentary angular deviation in azimuth and the other of said signals a measure of the momentary angular deviation in elevation between the direction of the second flying target and said line of sight; and after positioning the second electronic window at the image of the second flying target switching the actual value of the regulation system from the first pair of deviation signals to the second pair of deviation signals.
Claim 3
Dependent Claim
88 words
The method as defined in claim 1, further including the steps of: adding a respective azimuth additional signal and elevation additional signal to a respective one of the associated first deviation signals in order to position the second electronic window at the image of the second flying target; and simultaneously shifting the image device of the first electronic window through a deviation from the image center corresponding to the azimuth additional signal and the elevation additional signal, respectively, while the second electronic window remains at the image center.
Claim 4
Dependent Claim
53 words
The method as defined in claim 2, further including the steps of: starting from the value null changing the azimuth additional signal and the elevation additional signal until, owing to the reaction of a servo system of the regulation system to such change, there is approximately annihilated the respective associated second deviation signal.
Claim 5
Dependent Claim
30 words
The method as defined in claim 3, further including the steps of: selecting the duration of the changing operation to be appreciably greater than the time-constant of the regulation system.
Claim 6
Dependent Claim
53 words
The method as defined in claim 2, further including the steps of: employing the momentary position of the manually actuatable control means to determine the momentary value of the azimuth additional signal and the elevation additional signal; and both additional signals assuming the value null in a starting position of such control means.
Claim 7
Dependent Claim
76 words
The method as defined in claim 5, further including the steps of: changing the azimuth additional signal and the elevation additional signal starting from the value null, until owing to the reaction of a servo system of the regulation system to such change there is approximately annihilated the respective associated second deviation signal; and rendering ineffectual the manual actuatable control means at the moment of switching until it has been brought back into said starting position.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-07-02 | 1983-01-01 | 1983-07-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-07-02 | 1987-01-01 | 1987-07-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-07-02 | 1991-01-01 | 1991-07-03 | $7700.00 | Window Closed / Lapsed |