US4008470A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Passive ranging system
Assignee: United States Department of the Navy
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Filing: 1968-02-27
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Granted: 1977-02-15
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Expires: 1988-02-27
Abstract
Abstract A passive ranging system for determining the range of a target radar by uizing the scan characteristics of the target radar. Receivers are placed on each of two aircraft flying in a specified formation. One aircraft relays detected pulse amplitude envelopes to the other aircraft. The second aircraft measures time delay between impacts of the main beam of the target radar on the two aircraft and a computer determines range according to equation R=D/KΔt where Δt is the measured time difference, D is the distance between aircraft and K is a constant depending on the type of target radar.
Inventors
- 👤 George R. Lanning
- 👤 John Y. K. Chang
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 18:35
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/02; G01S13/06; G01S13/08; G01S1/00; G01S1/02
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
187 words
In a passive airborne ranging system for determining the range of target radars located on the surface of the earth, the combination comprising: a. first and second aircraft flying in a predetermined formation, each having radar receivers mounted therein for receiving energy signals radiated by a target radar of interest, b. said first aircraft having an envelope detector circuit means coupled to its radar receiver for detecting the envelope of the received radar signal, c. said first aircraft having a data link transmitter coupled to said first aircraft envelope detector for transmitting a signal modulated by the detected radar signal received by said first aircraft, d. said second aircraft having an envelope detector circuit means coupled to its radar receiver for detecting the envelope of the received radar signal, e. said second aircraft having data links receiving means for receiving and detecting the transmitted signal from said first aircraft, f. signal comparison means coupled to the envelope detector of said second aircraft and to said data link receiving means for producing an output signal proportional to the approximate range of the target radar to said second aircraft.
Claim 2
Dependent Claim
187 words
In a passive airborne ranging system for determining the range of target radars located on the surface of the earth, the combination comprising: a. first and second aircraft flying in a predetermined formation, each having radar receivers mounted therein for receiving energy signals radiated by a target radar of interest, b. said first aircraft having an envelope detector circuit means coupled to its radar receiver for detecting the envelope of the received radar signal, c. said first aircraft having a data link transmitter coupled to said first aircraft envelope detector for transmitting a signal modulated by the detected radar signal received by said first aircraft, d. said second aircraft having an envelope detector circuit means coupled to its radar receiver for detecting the envelope of the received radar signal, e. said second aircraft having data links receiving means for receiving and detecting the transmitted signal from said first aircraft, f. signal comparison means coupled to the envelope detector of said second aircraft and to said data link receiving means for producing an output signal proportional to the approximate range of the target radar to said second aircraft.
Claim 3
Dependent Claim
47 words
The ranging system of claim 1 wherein said signal comparison means includes visual means for determining the time delay between the time of arrival of the target radar signal at said first aircraft and the time of arrival of the target radar signal at said second aircraft.
Claim 4
Dependent Claim
25 words
The ranging system of claim 2 wherein the determined time delay is coupled as the only variable to a computing circuit to determine said range.
Claim 5
Dependent Claim
85 words
The ranging system of claim 2 wherein said signal comparison means includes: a. a divider circuit having a first input proportional to said time delay, a second input proportional to the distance between said aircraft and having an output, b. and a multiplier circuit having a first input coupled to the output of said divider circuit, a second input proportional to the angular scan rate of the target radar and producing an output signal proportional to the range of said aircraft to said target radar.
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) | 1980-02-15 | 1980-08-16 | 1981-02-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-02-15 | 1984-08-16 | 1985-02-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-02-15 | 1988-08-16 | 1989-02-15 | $7700.00 | Window Closed / Lapsed |