Refueling device

Patent metadata

Field	Value
Publication number	US-11465768-B2
Application number	US-201816623487-A
Country	US
Kind code	B2
Filing date	Jul 8, 2018
Priority date	Jul 10, 2017
Publication date	Oct 11, 2022
Grant date	Oct 11, 2022

Abstract

Computerized system and method of controlling a refueling device including, when the device is in a non-engaged state: receiving a first roll angle of a tanker, determining a first desired roll angle, and providing a command for controlling a roll element, thereby attempting to achieve or maintain a first roll angle that is substantially the same as the roll angle of the tanker. And, when the device is in an engaged state: receiving a second roll angle of the tanker, determining a second desired roll angle, and providing a command related to the desired roll angle for controlling a yaw element, thereby attempting to achieve or maintain a second roll angle that is substantially the same as the roll angle of the tanker, wherein the roll angle of the device during the engaged state is facilitated due to a degree of freedom between the refueling device body and refueling nozzle.

First claim

The invention claimed is:

1. A computerized method of controlling a refueling device, the method comprising:
(a) providing the refueling device that is attached by means of a non-rigid hose to a tanker aircraft; the refueling device having a refueling device body connected to a refueling nozzle by a joint, the joint facilitating at least a degree of freedom of the refueling device body relative to the refueling nozzle when the refueling nozzle is engaged with a receptacle of a receiver aircraft, constituting an engaged state;
(b) repeatedly performing by a controller:
in an instance which the refueling device is not engaged with the receiver aircraft, constituting a non-engaged state:
(b1) receiving a first roll angle of the tanker aircraft from the tanker aircraft;
(b2) determining a first desired roll angle of the refueling device based on the first roll angle of the tanker aircraft; and
(b3) providing a first one or more commands related to the first desired roll angle of the refueling device for controlling one or more roll elements of the refueling device thereby attempting to achieve or maintain a first roll angle of the refueling device that is substantially the same as the first roll angle of the tanker aircraft; and

in an instance which the refueling device is engaged with the receiver aircraft in said engaged state:
(b4) receiving a second roll angle of the tanker aircraft from the tanker aircraft;
(b5) determining a second desired roll angle of the refueling device based on the second roll angle of the tanker aircraft; and
(b6) providing a second one or more commands related to the second desired roll angle of the refueling device for controlling one or more yaw elements of the refueling device thereby attempting to achieve or maintain a second roll angle of the refueling device that is substantially the same as the second roll angle of the tanker aircraft; wherein the second roll angle of the refueling device during the engaged state is facilitated at least due to the degree of freedom between the refueling device body and the refueling nozzle.

2. The computerized method of claim 1 , wherein said stage (b3) is further comprising:
providing a first one or more commands related to the first desired roll angle of the refueling device for controlling said one or more yaw elements of the refueling device; and
wherein said stage (b6) is further comprising:
providing a second one or more commands related to the second desired roll angle of the refueling device for controlling said one or more roll elements of the refueling device;
thereby providing one or more commands to both the one or more roll elements and the one or more yaw elements seamlessly, irrespective of whether said refueling device is in said non-engaged state or said engaged state.

3. The computerized method of claim 1 , further comprising performing gain calibration to affect the first one or more commands and/or the second one or more commands provided to the one or more roll elements and/or the one or more yaw elements and thereby modify the effect that the one or more roll elements and/or the one or more yaw elements has when attempting to achieve the first and/or second desired roll angle.

4. The computerized method of claim 1 , wherein said stage (b2) is further comprising:
receiving a first roll angle of the refueling device and determining a first difference between the first desired roll angle and the first roll angle of the refueling device and utilizing said first difference for providing said first one or more commands; and
wherein said stage (b5) is further comprising:
receiving a second roll angle of the refueling device and determining a second difference between the second desired roll angle and the second roll angle of the refueling device and utilizing said second difference for providing said second one or more commands.

5. The computerized method of claim 1 , further comprising controlling the one or more roll elements and/or the one or more yaw elements based on the first and/or second one or more commands to attempt to achieve or maintain a roll angle of the refueling device that is substantially the same as the roll angle of the tanker aircraft.

6. The computerized method of claim 1 , wherein said stage (b2) and/or said stage (b5) is further comprising:
obtaining a relative position of the tanker aircraft and the refueling device;
obtaining a speed of the tanker aircraft; and
determining a side speed of the refueling device relative to the tanker based on the relative position of the tanker aircraft and the refueling device and the speed of the tanker aircraft; wherein the side speed of the refueling device relative to the tanker is used to prevent or reduce oscillation of the refueling device and thereby help to achieve or maintain a roll angle of the refueling device that is substantially the same as the roll angle of the tanker aircraft.

7. The computerized method of claim 1 , wherein said stage (b2) and/or said stage (b5) is further comprising obtaining a roll rate of the refueling device; wherein the roll rate is used to prevent or reduce oscillation of the refueling device and thereby help to achieve or maintain a roll angle of the refueling device that is substantially the same as the roll angle of the tanker aircraft.

8. The computerized method of claim 1 , wherein the refueling device is an unmanned aerial vehicle (UAV).

9. A non-transitory program storage device readable by machine, tangibly embodying a program of instructions executable by the machine to perform the method of controlling a refueling device according to claim 1 .

10. An inflight refueling system, comprising:
a refueling device that is attached by means of a non-rigid hose to a tanker aircraft; the refueling device having a refueling device body connected to a refueling nozzle by a joint, the joint facilitating at least a degree of freedom of the refueling device body relative to the refueling nozzle when the refueling nozzle is engaged with a receptacle of a receiver aircraft, constituting an engaged state;
a sensor configured to determine a roll angle of the tanker aircraft; and
a controller configured to repeatedly perform the following:
when the refueling device is not engaged with the receiver aircraft, constituting a non-engaged state:
(1) receive a first roll angle of the tanker aircraft from the tanker aircraft;
(2) determine a first desired roll angle of the refueling device based on the first roll angle of the tanker aircraft; and
(3) provide a first one or more commands related to the first desired roll angle of the refueling device to control one or more roll elements of the refueling device to thereby attempt to achieve or maintain a first roll angle of the refueling device that is substantially the same as the first roll angle of the tanker aircraft; and

when the refueling device is engaged with the receiver aircraft in said engaged state:
(4) receive a second roll angle of the tanker aircraft from the tanker aircraft;
(5) determine a second desired roll angle of the refueling device based on the second roll angle of the tanker aircraft; and
(6) provide a second one or more commands related to the second desired roll angle of the refueling device to control one or more yaw elements of the refueling device to thereby attempt to achieve or maintain a second roll angle of the refueling device that is substantially the same as the second roll angle of the tanker aircraft; wherein the second roll angle of the refueling device during the engaged state is facilitated at least due to the degree of freedom between the refueling device body and the refueling nozzle.

11. The inflight refue

Assignees

• Israel Aerospace Ind Ltd

Inventors

• Meidad Ido

Classifications

• B64U10/25

  Fixed-wing aircraft (VTOL aircraft B64U10/20) · CPC title

• B64D39/06 Primary

  Connecting hose to aircraft; Disconnecting hose therefrom · CPC title

• B64C13/02

  Initiating means · CPC title

• B64D39/00 Primary

  Refuelling during flight · CPC title

• B64C5/06

  Fins (B64C5/08 takes precedence) · CPC title