Patent US3921175A successfully refreshed from Google Patents.
← Back to Patent Explorer
US3921175A Expired / Lapsed US ⏱️ 0.0 years remaining

Method of monopulse angle gating for computer

Assignee: United States Department of the Navy
•
Filing: 1968-02-20
•
Granted: 1975-11-18
•
Expires: 1988-02-20
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A monopulse angle-gated guidance system consisting of a radio frequency receiver having an antenna, feed assembly and detectors, and a guidance computer including the basic computer and multiple target processing and scanning circuitry. A monopulse angle-gated guidance system for providing pursuitnavigation information to the servo system of an associated missile and provides a direction-finding information of radiating sources to a pilot.

Inventors

  • 👤 Richard S Hughes
  • 👤 James L Phillips

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-01 15:17
CPC Classifications
G; G01; G01S; G01S13/00; G01S13/02; G01S13/06; G01S13/42; G01S13/44; G01S13/4445; G01S3/00; G01S3/02; G01S3/14; G01S3/28; G01S3/32

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 238 words
A monopulse angle-gated computer for determining the direction of an energy radiating source comprising: receiver means for generating beam pairs having principle axes located in intersecting orthogonal planes; a servo-mechanism associated with each of said beam pairs and receiving the output of said receiver means corresponding to a beam pair and producing an error function dependent upon the voltage difference of each individual beam pair, said servo-mechanism being adapted to determine the angle to said energy radiating source, a further servo-mechanism coupled to each of said firstmentioned servo-mechanisms for normalizing the source signal strength from the error function of said first-mentioned servomechanisms, summing means included in said further servo-mechanism adapted to receive an input corresponding to each of said individual beams and having an output, gating means operative to interrupt the flow of information through the first-mentioned servo-mechanisms, said gating means having a predetermined reference threshold level so that signals at a given level below a reference will not allow operation of the first-mentioned servo-mechanisms, upper intensity discrimination means adapted to be actuated when the input signal is greater than a given level above the reference, the upper intensity discrimination corresponds to angle-gating, said further servo-mechanisms incorporating amplitude discrimination means, the input to said amplitude discriminating means comprising the difference pulses from the first-mentioned servo-mechanisms and a summation pulse from said last mentioned servo-mechanisms, and said amplitude discriminator operating to compare each difference pulse with the summation pulse.
Claim 2
Dependent Claim 238 words
A monopulse angle-gated computer for determining the direction of an energy radiating source comprising: receiver means for generating beam pairs having principle axes located in intersecting orthogonal planes; a servo-mechanism associated with each of said beam pairs and receiving the output of said receiver means corresponding to a beam pair and producing an error function dependent upon the voltage difference of each individual beam pair, said servo-mechanism being adapted to determine the angle to said energy radiating source, a further servo-mechanism coupled to each of said firstmentioned servo-mechanisms for normalizing the source signal strength from the error function of said first-mentioned servomechanisms, summing means included in said further servo-mechanism adapted to receive an input corresponding to each of said individual beams and having an output, gating means operative to interrupt the flow of information through the first-mentioned servo-mechanisms, said gating means having a predetermined reference threshold level so that signals at a given level below a reference will not allow operation of the first-mentioned servo-mechanisms, upper intensity discrimination means adapted to be actuated when the input signal is greater than a given level above the reference, the upper intensity discrimination corresponds to angle-gating, said further servo-mechanisms incorporating amplitude discrimination means, the input to said amplitude discriminating means comprising the difference pulses from the first-mentioned servo-mechanisms and a summation pulse from said last mentioned servo-mechanisms, and said amplitude discriminator operating to compare each difference pulse with the summation pulse.

References Cited (Backward Citations)

US3097356A Cited
US3340532A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1978-11-17 1979-05-19 1979-11-18 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1982-11-17 1983-05-19 1983-11-18 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1986-11-17 1987-05-19 1987-11-18 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag