GPS airborne target geolocating method

Abstract

A geolocation method is applied for accurate targeting of a target using an airborne beacon as a pseudo star generated by a high altitude vehicle, and using optical sensors by a low altitude vehicle for imaging the beacon and target for generating accurate relative GPS positioning of the target for improved the geolocation of the target preferably for precise delivery of a payload to the target. The method is applicable to military and civilian needs for accurate delivery of a payload to a target, such as for precise delivery of humanitarian aid or weapon munitions.

1. A method for determining a target location of a target, the method comprising the steps of,
 sensor determining a first GPS position of a sensor platform, the first GPS position having GPS positioning errors,    beacon determining a second GPS position of a beacon platform, the second GPS position having GPS positioning errors, the first and second GPS positions having relative errors less than the GPS positioning errors,    beacon measuring a beacon offset angle,    target measuring a target offset angle, and    computing the target location of the target from the first and second GPS positions and the beacon offset angle and the target offset angle.    
     
     
       2. The method of  claim 1  further comprising the steps of,
 determining a third GPS position of a maneuvering payload,    communicating the target location of the target to the maneuvering payload, and    maneuvering payload toward the target location.    
     
     
       3. The method of  claim 1  further comprising the steps of,
 determining a third GPS position of a maneuvering payload,    communicating the target location of the target to the maneuvering payload,    maneuvering payload toward the target location, and    repeating all of the steps for repetitively communicating the target location of the target to the maneuvering payload while the maneuvering payload maneuvers along a payload track towards the target.    
     
     
       4. The method of  claim 1 , wherein:
 the first GPS position has a y 1  altitude and an x 1  and a z 1  horizontal position, the second GPS position has a y 2  altitude and an x 2  and a z 2  horizontal position,    the beacon offset angle comprises the angle of φ x  and φ z ,    the target offset angle comprises the angles of θ x  and θ z , and    the target location is a horizontal location at x 2  and z 3 .    
     
     
       5. The method of  claim 1  wherein,
 the first GPS position has a Y 1  altitude and an x 1  horizontal position, the second GPS position has a Y 2  altitude and an x 2  horizontal position,    the beacon offset angle comprises the angle of φ x ,    the target offset angle comprises the angles of φ x , and    the target location is a horizontal location at x 3 , where x 3 y 1  tan[θ x +φ x −α x ] where α x =arctan(x 2 /(y 2 −y 1 )).    
     
     
       6. The method of  claim 1  wherein the beacon maneuvering step comprises the step of,
 calibrating a focal plane of a beacon sensor of the sensor platform for measuring the beacon offset angle.    
     
     
       7. The method of  claim 1  wherein the target measuring step comprises the step of,
 calibrating a focal plane of a target sensor of the sensor platform for measuring the target offset angle.    
     
     
       8. The method of  claim 1  wherein,
 the beacon measuring step comprises the step of calibrating a beacon focal plane of a beacon sensor of the sensor platform for measuring the beacon offset angle,    the target measuring step comprises the step of calibrating a target focal plane of a target sensor of the sensor platform for measuring the target offset angle, and    the calibrating of the beacon and target focal plane is relative to respective fields of view of a common boresight.    
     
     
       9. A method for delivering a payload to a target location of a target, the method comprising the steps of,
 determining a first GPS position of a sensor platform,    determining a second GPS position of a beacon platform, the first and second GPS positions having relative errors,    measuring a beacon offset angle,    measuring a target offset angle,    computing the target location of the target from the first and second GPS position and beacon offset angle and target offset angle,    determining a third GPS position of a maneuvering payload,    communicating the target location to the maneuvering payload, and    maneuvering payload toward to the target location for delivering the payload to the target location.    
     
     
       10. The method of  claim 9  wherein maneuvering payload is a smart bomb comprising GPS navigation, guide communications, and a munitions payload. 
     
     
       11. A method for providing a navigational beacon to a sensor platform, comprising:
   outputting a beacon from a moving beacon platform at a first GPS position;        receiving the beacon from the moving beacon platform at the sensor platform, wherein the sensor platform is at a second GPS position at a lower altitude with respect to the moving beacon platform;        imaging the beacon; and        storing the location of the beacon.      
     
     
       12. The method of  claim 11 , wherein the beacon is a narrow directional beam.  
     
     
       13. The method of  claim 12 , wherein the narrow directional beam is a laser.  
     
     
       14. The method of  claim 13 , wherein the laser wavelength comprises at least one of a visible wavelength, an ultraviolet wavelength, and an infrared wavelength.  
     
     
       15. The method of  claim 11 , wherein the moving beacon platform comprises an airborne unmanned vehicular system.  
     
     
       16. The method of  claim 11 , wherein the sensor platform comprises an airborne unmanned vehicular system.  
     
     
       17. The method of  claim 11 , wherein the beacon is encrypted.