Use of bistatic radar system for determining distance between airborne aircraft

• US 4,370,656 A
• Filed: 10/27/1980
• Issued: 01/25/1983
• Est. Priority Date: 10/27/1980
• Status: Expired due to Term

• Current Assignee: Hughes Missile Systems Company
• Original Assignee: General Dynamics
• Inventors: Lewis, Benjamin G., Frazier, Lawrence M.
• Primary Examiner(s): Tubbesing, T. H.
• Application Number:
  US06/200,660
• Time in Patent Office: 820 Days
• Field of Search: 343/12 R, 343/112 D
• US Class Current: 342/458
• CPC Class Codes: G01S 11/04 using angle measurements
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 5/0273 using multipath or indirect path propagation signals in position determination
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

A bistatic passive radar system and method for airborne use in a first aircraft in conjunction with a host transmitter located in a second aircraft that may be at a different altitude than the first aircraft, characterized by a system and method for determining the distance between the aircraft. The system for determining the distance between the aircraft includes a system for receiving radar signals from the host transmitter directly and via reflection from a selected ground target located between the two aircraft; a system coupled to the receiver for determining the apparent range R_a from the host transmitter on the second aircraft to the receiver on the first aircraft in response to receipt of the radar signals; a device on the first aircraft for determining the altitude H of the first aircraft; a device on the first aircraft for determining the angle θ with respect to vertical at which the radar signals are received directly from the host transmitter; a device on the first aircraft for determining the angle φ with respect to vertical at which the reflected radar signals from the ground are received; and a computer system on the first aircraft for computing the distance D between the two aircraft from the determined values of R_a, H, θ and φ. The system further includes an alphanumeric display device coupled to the computer system for providing an alphanumeric readout of the computer value of the distance D between the aircraft.

Claims

1. A bistatic passive radar system for airborne use in a first aircraft in conjunction with a host transmitter located in a second aircraft that may be at a different altitude than the first aircraft, characterized by means for determining the distance between the aircraft comprising

means for receiving radar signals from the host transmitter directly and via reflection from a selected ground target located between the two aircraft;

means coupled to the receiving means for determining the apparent range R_a from the host transmitter to the receiving means in response to receipt of said radar signals;

means for determining the altitude H of the first aircraft;

means for determining the angle θ

with respect to vertical at which the radar signals are received directly from the host transmitter and for determining the angle φ

with respect to vertical at which the reflected radar signals are received; and

means for computing the distance D between the aircraft from the determined values of R_a, H, θ and

φ

.

2. A system according to claim 1, wherein the computing means comprises means for computing the vertical angle B between the line of sight from ther first aircraft to the second aircraft and a line from the ground target to the first aircraft by computing the difference between the determined values of θ

and φ

;

means for computing the distance C from the ground target to the first aircraft by dividing the determined value of the altitude H by cosine φ

; and

means for computing the distance D between the aircraft in accordance with the equation;

##EQU2##

3. A system according to claims 1 or 2 further comprising means coupled to the computing means for providing an alphanumeric readout of the computed value of the distance D between the aircraft.

4. A method of using a bistatic passive radar system located in a first airborne aircraft in conjunction with a host transmitter located in a second airborne aircraft that may be at a different altitude than the first aircraft, characterized by determining the distance between the aircraft by the steps of:

(a) receiving radar signals from the host transmitter directly and via reflection from a selected ground target located between the two aircraft;

(b) determining the apparent range R_a from the host transmitter to the first aircraft in response to receipt of said radar signals;

(c) determining the altitude H of the first aircraft;

(d) determining the angle θ

with respect to vertical at which the radar signals are received directly from the host transmitter;

(e) determining the angle φ

with respect to vertical at which the reflected radar signals are received; and

(f) computing the distance D between the aircraft from the determined values of R_a, H, θ and

φ

.

5. A method according to claim 4, wherein step (f) comprises the steps of

(g) computing the vertical angle B between the line of sight from the first aircraft to the second aircraft and a line from the ground target to the first aircraft by computing the difference between the determined values of θ

and φ

;

(h) computing the distance C from the ground target to the first aircraft by dividing the determined value of the altitude H by cosine φ

; and

(i) computing the distance D between the aircraft in accordance with the equation;

##EQU3##

6. A method according to claims 4 or 5 further comprising the step of

(j) providing an alphanumeric readout of the computed value of the distance D between the aircraft.