Passive-type range determining system using scanning receiving devices

• US 4,339,755 A
• Filed: 03/03/1980
• Issued: 07/13/1982
• Est. Priority Date: 03/03/1980
• Status: Expired due to Term

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Wright, James M.
• Primary Examiner(s): Hubler, Malcolm F.
• Application Number:
  US06/126,456
• Time in Patent Office: 862 Days
• Field of Search: 343/118, 343/15, 343/13 R, 343/112 D, 364/458
• US Class Current: 342/458
• CPC Class Codes: G01S 11/04 using angle measurements
• CPC Class Codes: G01S 5/04 Position of source determined by a plurality of spaced direction-finders

Abstract

A pair of scanning, directional receiving antennas mounted in spaced relation on a monitoring aircraft are synchronously driven at a given scan rate ω_s and at the same phase angle with respect to the broadside of the antenna pair so that the receiving beams of the antennas are always parallel. A non-scanning source of RF radiation, located at an unknown range from the monitoring aircraft, emits radiation that is received by the scanning antennas at a slight time differential t₂₁. The received source radiation is converted by separate receiving channels into early and late arriving signals, from which a time interval signal representing t₂₁ is produced. Concurrently therewith, an angle of arrival φ of the source radiation is detected and a signal representative thereof is produced. Also, signals are generated that represent the scan rate ω_s of the receiving antennas and a distance d equal to the separation between the antennas. From these signals, a range signal R is produced that corresponds to the distance between the monitoring aircraft and the source of RF radiation.

Claims

1. An apparatus for determining the range of a source of electromagnetic transmission from a monitoring location, comprising:

first and second directional receiving means each having a principal receiving axis for receiving the transmission when said axes are aligned with the source, said first and second receiving means being arrayed at relatively spaced-apart positions separated by a distance d at said monitoring location, and means for mounting said first and second receiving means for scanning;

scan driver means for causing each of said first and second receiving means to scan at a predetermined scan rate ω

_s and in phase synchronization so that any instant both said receiving means are oriented at the same angle α

with respect to the broadside of said receiving means, and so that the principal receiving axes of said first and second receiving means are parallel;

first and second channel electrical means connected to said first and second receiving means, respectively, for developing early and late arriving signals representing the receipt by said first and second receiving means of the transmission;

means for measuring a time differential t₂₁ between early and late arriving signals developed by said first and second channel electrical means, and for producing a signal representing said time differential t₂₁ ;

angle of arrival measurement means for measuring an angle φ

at which the transmission arives at said monitoring location relative to said receiving means, and for producing a signal representing said angle φ

; and

,

range determining circuit means responsive to said signals representing said time differential t₂₁ and said angle of arrival φ

, for producing an output signal proportional to the range as a function of said signals representing said time differential t₂₁, said angle of arrival φ

, said separation distance d and said scan rate ω

_s.

2. The apparatus of claim 1 wherein said source produces electromagnetic transmission of radio frequencies, and wherein said first and second directional receiving means each comprise directional antennas for receiving radio frequencies.

3. The apparatus of claim 1 wherein the monitoring location is provided by a monitoring aircraft, and wherein the apparatus is effective to passively determine said range without requiring manuevers by the monitoring aircraft, and wherein the apparatus further comprises means for mounting said first and second receiving means on said monitoring aircraft separated by said distance d.

4. The apparatus of claim 3 wherein said means for mounting said first and second receiving means on said monitoring aircraft further comprises means for mounting said first and second receiving means on opposed wings of said aircraft.

5. The apparatus of claim 1 wherein said range determining circuit means comprises means responsive to said angle of arrival detector means for producing a signal representing d cos φ

; and

means responsive to said means for measuring said time differential for producing a signal representing t₂₁ ω

_s ; and

means for dividing said signal representing d cos φ

by said signal representing t₂₁ ω

_s.

6. The apparatus of claim 1, wherein said scan driver means includes means for producing a signal representing said scan rate ω

_s, and wherein said range determining circuit means comprises function generator means responsive to said angle of arrival detector means for producing a signal representing d cos φ

, and multiplier means responsive to said means for measuring said time differential and to said means for producing said signal representing said scan rate ω

_s for multiplying such signals to produce a signal representing t₂₁ ω

_s, and divider means for dividing said signal representing d cos φ

by said signal representing t₂₁ ω

_s.

7. The apparatus of claim 1 wherein said range determining circuit means comprises signal processing means for producing said output signal as the following function of said signals representing said time differential t₂₁, said angle of arrival φ

, said separation distance d and said scan rate ω

_s ;

space="preserve" listing-type="equation">R=(d cos φ

)/(t.sub.2 ω

.sub.s)

where R represents said output signal proportional to the range.

8. A method for determining the range of a source of electromagnetic transmission from a monitoring location, comprising the steps of:

scanning first and second spaced-apart, directional receiving devices, which are sensitive to said electromagnetic transmission, at the same scan rate ω

_s and in phase synchronization so that the principal directional receiving axes of said first and second receiving devices are maintained parallel;

developing early and late arriving signals in response to the receipt by said first and second receiving devices of the electromagnetic transmission;

resolving a time differential t₂₁ between the early and late arriving signals;

detecting an angle of arrival φ

at which the electromagnetic transmission arrives at said monitoring location; and

,

producing an output signal representing the range between said monitoring location and said source of electromagnetic transmission as a function of said resolved time differential t₂₁, said scan rate ω

_s, a distance d separating said first and second receiving devices, and the detected angle of arrival φ

.

9. The method of claim 8 wherein said monitoring location is on a monitoring aircraft, and said first and second receiving devices are mounted on said monitoring aircraft at a separation distance d for passively determining the range to a distant source of transmission without requiring maneuvers by said monitoring aircraft.

10. The method of claim 8 wherein said step of determining said range comprises the substeps of:

generating an electrical signal representing the function d cos φ

in response to the step of detecting the angle of arrival φ

;

producing a signal representing the time differential t₂₁ ω

_s in response to the step of resolving said time differential t₂₁ ; and

,

dividing the signal representing d cos φ

by the signal representing t₂₁ ω

_s to produce a signal representing the range R.