Missile tracking by GPS reflections

• US 8,610,041 B1
• Filed: 05/23/2011
• Issued: 12/17/2013
• Est. Priority Date: 05/23/2011
• Status: Expired due to Fees

• Current Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Original Assignee: Lockheed Martin Corporation (Martin Marietta Corporation)
• Inventors: Boardman, Jonathan A.
• Primary Examiner(s): GREGORY, BERNARR E
• Application Number:
  US13/113,487
• Time in Patent Office: 939 Days
• Field of Search: 244 31- 33, 89/11.1, 701/1, 701/3, 701/4, 701/400, 701/408, 701/467, 701/468, 342 25 R- 25 F, 342 61- 68, 342104-115, 342/118, 342/146, 342/147, 342/175, 342192-197, 342/350, 342/352, 342/357.2, 342/357.21, 342/357.22, 342/357.25, 342/357.31, 342/357.32, 342/357.39, 342/357.4, 342/357.51, 342/357.52, 342/357.61, 342/351
• US Class Current: 244/3.19
• CPC Class Codes: F41G 7/2253 Passive homing systems, i.e. comprising a receiver and do not requiring an active illumination of the target
• CPC Class Codes: F41G 7/2286 using radio waves
• CPC Class Codes: F42B 15/01 Arrangements thereon for guidance or control steering arrangements F42B10/60; aircraft flight control B64C; guidance systems other than those installed aboard F41G7/00, F41G9/00; locating by use of radio or other waves G01S; flight control in general G05D1/00; computer aspects G06]
• CPC Class Codes: G01S 13/003 Bistatic radar systems; Multistatic radar systems
• CPC Class Codes: G01S 13/878 Combination of several spaced transmitters or receivers of known location for determining the position of a transponder or a reflector G01S13/874 takes precedence
• CPC Class Codes: G01S 13/883 for missile homing, autodirectors missile guidance systems F41G7/22

Abstract

A system for engaging hostile air or space threats with a defensive missile, where the defensive missile comprises an antenna for receiving global positioning system (GPS) signals. A global positioning system receiver is coupled to said antenna, for receiving global positioning system signals directly from global positioning system satellites and global positioning system signals reflected from the threat. A processing arrangement processes the direct and reflected global positioning system signals for determining the position and velocity of the threat. Vectoring controls are coupled to the processing arrangement, and are responsive to the location of the threat for directing the defensive missile toward the threat. In a particular embodiment, the antenna of the defensive missile is directionally controllable, and the defensive missile includes an antenna direction controller responsive to the processor for directing at least a beam of the antenna toward the threat.

Claims

1. A system for engaging an air or space target, said system comprising:

a missile equipped with an antenna capable of receiving global positioning system (GPS) signals;

a global positioning system receiver coupled to said antenna, for receiving global positioning system signals directly from global positioning system satellites and global positioning system signals reflected from the target;

a processing arrangement for processing said direct and reflected global positioning system signals for determining the state of the target; and

vectoring controls coupled to said processing arrangement, and responsive to said state of the target for directing said missile toward the target.

2. A system according to claim 1, wherein:

said antenna is capable of being controllably beamsteered; and

said processing arrangement is coupled to said antenna for directing a beam of said antenna toward said position of said target.

3. A system according to claim 2, wherein said processing arrangement includes a cue signal function which responds to a target cueing signal for directing said beam of said antenna in the cue direction.

4. A system according to claim 2, wherein said processing arrangement includes a function responsive to a lack of a target cue signal, for scanning said beam over a region of space in a search pattern.

5. A system according to claim 1, wherein said antenna is directionally controllable, and said missile further includes an antenna beam direction controller coupled to said antenna and to said processing arrangement for directing a beam of said antenna generally toward said position of said target.

6. A system according to claim 1, wherein the state of the target comprises the position and velocity of the target.

7. A method for engaging an elevated target, said method comprising the steps of:

launching a missile upon the approach of the target, said missile including an antenna array and a global positioning system signal processor;

activating said antenna and said global positioning system signal processor;

acquiring and tracking global positioning system signals flowing directly from global positioning system satellites to the missile;

determining from said global positioning system signals flowing directly from the global positioning system satellites a solution for the location of said missile;

acquiring and tracking global positioning system signals flowing from global positioning system satellites to the target, and reflecting from said target toward said missile;

from said global positioning system signals flowing from global positioning system satellites to the target, and reflecting from said target toward said missile, generating a solution for the state of said target; and

guiding said missile to intercept said target.

8. A method according to claim 7, wherein the step of generating a solution for the state of the target comprises generating a solution for the position and velocity of the target.