초록 ▼

A system and method for refueling unmanned aerial vehicles. The system is adapted to refuel a first unmanned aerial vehicle from a second unmanned aerial vehicle and includes an arrangement for flying the first and second vehicles to proximity within a predetermined range and for connecting an umbil

A system and method for refueling unmanned aerial vehicles. The system is adapted to refuel a first unmanned aerial vehicle from a second unmanned aerial vehicle and includes an arrangement for flying the first and second vehicles to proximity within a predetermined range and for connecting an umbilical from the second vehicle to the first vehicle in flight. In the illustrative embodiment, the arrangement for connecting includes a targeting system for electromagnetically detecting a refueling receptacle on the first vehicle. The targeting system includes a first coil around a refueling receptacle on the first vehicle. A seeker is disposed at a first end of said umbilical on the second vehicle. The seeker includes three detector coils adapted to detect a magnetic signal from the first coil around the receptacle on the first vehicle. The coils are mounted such that the detector coils point in different directions. The outputs of the coils are processed to determine the direction and range to the UAV from the tanker UAV.

대표청구항 ▼

What is claimed is: 1. A system for refueling a first unmanned aerial vehicle from a second unmanned aerial vehicle comprising: means for flying said first and second vehicles to proximity within a predetermined range; means for connecting an umbilical from one vehicle to the other vehicle in fligh

What is claimed is: 1. A system for refueling a first unmanned aerial vehicle from a second unmanned aerial vehicle comprising: means for flying said first and second vehicles to proximity within a predetermined range; means for connecting an umbilical from one vehicle to the other vehicle in flight, said means for connecting including a targeting system for magnetically detecting a refueling receptacle coupled to said first vehicle, said targeting system including: a first coil disposed around said refueling receptacle on said first vehicle, second coil disposed around said receptacle on said first vehicle means for exciting said first and second coils with first and second respective signals at first and second separate and distinct frequencies, a seeker disposed at a first end of said umbilical on said second vehicle, said seeker including first and second detector coils adapted to detect a magnetic signal from said first and said second coils, logic means for receiving a signal output by at least one of said detector coils and determining a direction and a range to said receptacle from said umbilical in response thereto. 2. The invention of claim 1 including means for retaining said detector coils such that a first detector coil points in a first direction, said second detector coil points in a second direction and a third detector coil points in a third direction. 3. A system for refueling a first unmanned aerial vehicle from a second unmanned aerial vehicle comprising: means for flying said first and second vehicles to proximity within a predetermined range; means for connecting an umbilical from one vehicle to the other vehicle in flight, said means for connecting including a targeting system for magnetically detecting a refueling receptacle coupled to said first vehicle, said targeting system including: a first coil disposed around a refueling receptacle on an umbilical extending from said first vehicle; a second coil disposed around said receptacle on said umbilical; means for exciting said first and second coils with first and second respective signals at first and second separate and distinct frequencies; a seeker disposed on said second vehicle, said seeker including first and second detector coils adapted to detect a magnetic signal from said first and said second coils; and logic means for receiving a signal output by at least one of said detector coils and determining a direction and a range to said receptacle from said umbilical in response thereto. 4. The invention of claim 1 wherein said means for flying includes a precision guidance system. 5. The invention of claim 4 wherein said guidance system includes means for determining the position and velocity of said first and said second vehicles. 6. The invention of claim 5 wherein said guidance system includes means for commanding said first and second vehicles into a predetermined flight pattern.