Passive ranging using global positioning system

• US 6,150,979 A
• Filed: 11/30/1998
• Issued: 11/21/2000
• Est. Priority Date: 11/30/1998
• Status: Expired due to Fees

• Current Assignee: The United States of America As Represented By The Secretary of Agriculture
• Original Assignee: United States Of America As Represented By The Secretary Of The Air Force
• Inventors: Tsui, James B. Y.
• Primary Examiner(s): Tarcza, Thomas H.
• Assistant Examiner(s): PHAN, DAO LINDA
• Application Number:
  US09/201,554
• Time in Patent Office: 722 Days
• Field of Search: 342/357.06, 342/357.08, 342/126, 701/213
• US Class Current: 342/357.61
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 19/18 Military applications
• CPC Class Codes: G01S 5/12 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Abstract

A method for determining distance from a target to an observation station using a Global Positioning System satellite as a radiation source and first and second observation station located receivers. The first receiver receives reflected position determinative satellite radio frequency signals and the second receiver receives direct position determinative satellite radio frequency signals. The time difference between satellite radio frequency signals arriving at the first and second receivers is calculated and combined with difference distance data and angular, azimuth and elevational position data and the distance from the target to observation point is determined.

Claims

1. A method for determining distance from a target to an observation station using a Global Positioning System satellite as a radiation source, said method comprising the steps of:

pointing an observation station located first receiver directional antenna toward said target and receiving reflected position determinative satellite radio frequency signals therefrom;

positioning an observation station located second receiver toward said satellite and receiving position determinative satellite radio frequency signals therefrom;

determining a time difference between satellite radio frequency signals arriving at said second receiver directional antenna and reflected satellite radio frequency signals arriving at said first receiver;

measuring angular position α

between said satellite and said target relative to said observation station using data obtained from said pointing, positioning and determining steps; and

calculating the distance from said target to said observation station using triangulation mathematics and data obtained from said pointing, positioning and calculating steps.

2. The method of claim 1 for determining distance to a target from an observation station wherein said pointing step further includes pointing an observation station located first receiver directional antenna toward said target using conventionally obtained angle of arrival data.

3. The method of claim 1 for determining distance to a target from an observation station wherein said calculating step further includes calculating the distance d using the equation ##EQU3## where m=a+d, m being the measured difference distance between said satellite and said target and between said satellite and said observation station, and a=d cos β

represents distance from said satellite to said target, β

=180°

-cos α

, cos α

=u•

d, where •

represents dot product and u is represented by u=cos φ

cos θ

x+cos φ

sinθ

y+sin φ

z, φ and

θ

representing elevation and azimuth angle of said satellite relative to said observation station.

4. A method for determining distance from a target to an observation station using a plurality of Global Positioning System satellites as radiation sources, said method comprising the steps of:

pointing an observation station located first receiver directional antenna toward said target and receiving reflected position determinative satellite radio frequency signals therefrom;

positioning an observation station located second receiver toward said satellites and receiving position determinative satellite radio frequency signals therefrom;

calculating a time difference between satellite radio frequency signals arriving at said second receiver directional antenna and reflected satellite radio frequency signals arriving at said first receiver;

measuring angular position α

between said satellites and said target relative to said observation station using data obtained from said pointing, positioning and calculating steps; and

calculating with least square mathematics the distance from said target to said observation station using triangulation mathematics and data obtained from said pointing, positioning and calculating steps.

5. The method of claim 4 for determining distance to a target from an observation station wherein said pointing step further includes pointing an observation station located first receiver directional antenna toward said target using conventionally obtained angle of arrival data.

6. The method of claim 4 for determining distance to a target from an observation station wherein said calculating step further includes calculating the distance d using the equation