Autonomous precision weapon delivery using synthetic array radar

• US 5,260,709 A
• Filed: 12/19/1991
• Issued: 11/09/1993
• Est. Priority Date: 12/19/1991
• Status: Expired due to Term

• Current Assignee: Raytheon Company (Rtx Corporation)
• Original Assignee: Hughes Aircraft Company (Rtx Corporation)
• Inventors: Nowakowski, Michael V.
• Primary Examiner(s): Sotomayor, John B.
• Application Number:
  US07/810,630
• Time in Patent Office: 691 Days
• Field of Search: 342/62, 342/63, 342/64, 342/95, 342/97, 342/357, 342/25, 244/3.2
• US Class Current: 342/62
• CPC Class Codes: F41G 7/007 Preparatory measures taken before the launching of the guided missiles
• CPC Class Codes: F41G 7/346 using global navigation satellite systems, e.g. GPS, GALILEO, GLONASS
• CPC Class Codes: F41G 7/36 using inertial references

Abstract

A system and method that uses differential computation of position relative to a global positioning system (GPS) coordinate system and the computation of an optimum weapon flight path to guide a weapon to a non-moving fixed or relocatable target. The system comprises an airborne platform that uses a navigation subsystem that utilizes the GPS satellite system to provide the coordinate system and a synthetic array radar (SAR) to locate desirable targets. Targeting is done prior to weapon launch, the weapon therefore requires only a navigation subsystem that also utilizes the GPS satellite system to provide the same coordinate system that the platform used, a warhead and a propulsion system (for powered weapons only). This results in a very inexpensive weapon with a launch and leave (autonomous) capability. The computational procedure used in the platform uses several radar measurements spaced many degrees apart. The accuracy is increased if more measurements are made. The computational algorithm uses the radar measurements to determine the point in a plane where the target is thought to be and the optimum flight path through that point. The weapon is flown along the optimum flight path and the impact with the ground results in a very good CEP when a sufficient number of radar measurements are made. The present invention provides fully autonomous, all-weather, high precision weapon delivery while achieving a relatively low cost. High precision weapon guidance is provided by the unique differential guidance technique (if a sufficiently accurate and stable navigation system is used).

Claims

1. An autonomous weapon targeting and guidance system for identifying a non-moving fixed or relocatable target and guiding a weapon to the target, said system comprising:

an airborne platform comprising a synthetic array radar (SAR) system adapted to detect a non-moving, fixed or relocatable target, a navigation subsytem, and processing means for processing SAR data and navigation data to compute the position of the target and an optimum weapon flight path from the platform to the target using a predetermined computational procedure; and

a weapon having a navigation subsystem which utilizes a transfer alignment algorithm to align the weapon'"'"'s navigation system with the airborne platform'"'"'s navigation system prior to launch, which weapon is adapted to respond to data transferred to it by the platform to permit it to navigate relative to the navigation system of the airborne platform and autonomously navigate to the location of the target along the optimum weapon flight path.

2. The system of claim 1 wherein the navigation subsystems of the airborne platform and weapon are each adapted to utilize a global positioning system (GPS) satellite system.

3. The system of claim 1 wherein the airborne platform is adapted to transfer target position, satellite, and flight path information to the weapon prior to its launch for use by the weapon during its flight along the optimum weapon flight path to the target.

4. The system of claim 2 wherein the airborne platform is adapted to transfer target position, satellite, and flight path information to the weapon prior to its launch for use by the weapon during its flight along the optimum weapon flight path to the target.

5. The system of claim 1 wherein the target is a fixed target.

6. The system of claim 1 wherein the target is a relocatable target.

7. An autonomous weapon targeting and guidance system for identifying a non-moving target and guiding a weapon to the target, said system comprising:

a global positioning system (GPS) comprising a plurality of satellites that broadcast position data to provide a coordinate reference frame;

an airborne platform comprising a synthetic array radar (SAR) system adapted to detect a non-moving target, a navigation subsystem that utilizes a global positioning system (GPS) satellite system and which is adapted to respond to signals provided by the GPS satellite system to permit the platform to navigate relative thereto, and processing means for processing SAR data and navigation data to compute the position of the target and an optimum weapon flight path from the platform to the target using a predetermined computational procedure; and

a weapon comprising a navigation subsystem that is adapted to utilize the GPS satellite system and which responds to signals provided by the GPS satellite system and data transferred to it by the platform to permit it to navigate relative to the GPS satellite system and autonomously navigate to the location of the target along the optimum weapon flight path.

8. The system of claim 7 wherein the airborne platform is adapted to transfer target position, satellite, and flight path information to the weapon prior to its launch for use by the weapon during its flight along the optimum weapon flight path to the target.

9. A method for detecting a non-moving target and guiding an airborne weapon to the target, said method comprising the steps of:

providing a global positioning system comprised of a plurality of satellites that each broadcast coordinate reference data for use in navigation;

flying an airborne platform over a target area and navigating using a navigation system that utilizes the GPS satellite system which provides the coordinate reference frame;

mapping the target area using a synthetic array radar (SAR) system located on the airborne platform to produce an original SAR map of the target area;

designating a target on the SAR map;

re-mapping the target area a predetermined number of additional times at different angles relative to the target using the synthetic array radar system to produce a predetermine number of additional SAR maps of the target area;

computing a precise target location and flight path in the coordinate system provided by the global positioning system using the navigation data and the information from each of the SAR maps;

transferring selected information to the weapon prior to its launch comprising data indicative of an optimum flight path to the target that should be flown by the weapon, navigation system initialization information that permits the weapon to acquire the satellites used by the platform for navigation, and target position information; and

launching the weapon using a navigation system in the weapon to acquire the satellites used by the platform for navigation and guide the weapon to the target based on the optimum flight path computed in the platform.

10. The method of claim 9 which further comprises the step of correlating the images from the additional SAR maps with the original SAR map prior to computing the precise target location and flight path to eliminate the need for repeated target designation.

11. The method of claim 9 which further comprises the step of providing target cueing information that is adapted to assist an operator in designating a target.

12. The method of claim 9 which further comprises the step of matching subsequent SAR maps to the initial SAR map by automatically determining a coordinate transformation that aligns all SAR images to ensure that the additional SAR maps are correlated to the initial SAR map, such that the target designated in each subsequent map is the same target designated in the first map.

13. A method for detecting a non-moving target and guiding an airborne weapon to the target, said method comprising the steps of:

providing a global positioning system comprised of a plurality of satellites that each broadcast coordinate reference data for use in navigation;

flying an airborne platform over a target area and navigating using a navigation system that utilizes the GPS satellite system which provides the coordinate reference frame;

mapping the target area using a synthetic array radar (SAR) system located on the airborne platform to produce an original SAR map of the target area;

designating a target on the SAR map;

re-mapping the target area a predetermined number of additional times at different angles relative to the target using the synthetic array radar system to produce a predetermine number of additional SAR maps of the target area;

correlating the images from the additional SAR maps with the original SAR map to eliminate the need for repeated target designation;

computing a precise target location and flight path in the coordinate system provided by the global positioning system using the navigation data and the information from each of the SAR maps;

transferring selected information to the weapon prior to its launch comprising data indicative of an optimum flight path to the target that should be flown by the weapon, navigation system initialization information that permits the weapon to acquire the satellites used by the platform for navigation, and target position information; and

launching the weapon using a navigation system in the weapon to acquire the satellites used by the platform for navigation and guide the weapon to the target based on the optimum flight path computed in the platform.