GPS airborne target geolocating method

• US 6,535,816 B1
• Filed: 06/10/2002
• Issued: 03/18/2003
• Est. Priority Date: 06/10/2002
• Status: Expired

• Current Assignee: Aerospace Corporation
• Original Assignee: Aerospace Corporation
• Inventors: Smith, Patrick Lawrence
• Primary Examiner(s): Camby, Richard M.
• Application Number:
  US10/166,525
• Time in Patent Office: 281 Days
• Field of Search: 701/213, 701/207, 701/214, 701/215, 701/222, 701/225, 701/200, 701/205, 701/206, 731/78.R, 333/00, 333/04, 333/13, 342/385, 342/386, 342/149, 342/152, 342/387
• US Class Current: 701/213
• CPC Class Codes: G01S 19/51 Relative positioning
• CPC Class Codes: G01S 5/16 using electromagnetic waves other than radio waves

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.

Claims

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 y₁ altitude and an x₁ and a z₁ horizontal position, the second GPS position has a y₂ altitude and an x₂ and a z₂ 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 x₃ and z₃.

5. The method of claim 1 wherein,

the first GPS position has a Y₁ altitude and an x₁ horizontal position, the second GPS position has a Y₂ altitude and an x₂ horizontal position,

the beacon offset angle comprises the angle of φ

_x,

the target offset angle comprises the angles of θ

_x, and

the target location is a horizontal location at x₃, where x₃y₁ tan[θ

_x+φ

_x−

α

_x] where α

_x=arctan(x₂/(y₂−

y₁)).

6. The method of claim 1 wherein the beacon measuring 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.