AUTONOMOUS HELICOPTER POSTURE REGULATION TO MOVING REFERENCE FRAMES

• US 20180059689A1
• Filed: 09/01/2017
• Published: 03/01/2018
• Est. Priority Date: 09/01/2016
• Status: Active Grant

• Current Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Original Assignee: Sikorsky Aircraft Corporation (Martin Marietta Corporation)
• Inventors: Flickinger, Daniel Montrallo, Ward, Mark D., McNeill, William T.
• Granted Patent: US 10,459,456 B2
• Time in Patent Office: Days
• CPC Class Codes: B64D 1/22 Taking-up articles from earth's surface
• CPC Class Codes: G05D 1/0088 characterized by the autonomous decision making process, e.g. artificial intelligence, predefined behaviours using knowledge based models G06N5/00
• CPC Class Codes: G05D 1/0684 on a moving platform, e.g. aircraft carrier
• CPC Class Codes: G05D 1/12 Target-seeking control

Abstract

A system and method for flying an aircraft is disclosed. A perception system at the aircraft tracks a trajectory of a moving object. A processor determines, from the trajectory of the moving object, a reference frame in which the moving object is stationary and establishes the aircraft at a selected offset from the moving object for the trajectory of the moving object. The aircraft is flown along a flight path based on the selected offset using calculations performed with respect to the determined reference frame.

Claims

1. A method of flying an aircraft, comprising:

determining a trajectory of a moving object relative to the aircraft;

determine, from the trajectory of the moving object, a reference frame in which the moving object is stationary;

flying the aircraft via a processor to maintain the aircraft at a selected offset from the moving object for the determined trajectory of the moving object; and

implementing a flight command to fly the aircraft along a flight path using calculations performed with respect to the determined reference frame.

2. The method of claim 1, wherein flying the aircraft along the flight path further comprises landing one of the aircraft and an item conveyed by the aircraft on the moving object.

3. The method of claim 1, further comprising tracking a rotation of the moving object about an axis of the moving object and correcting the flight path for the rotation of the moving object.

4. The method of claim 3, further comprising mimicking the rotation of the moving object at one of the aircraft and a slung load conveyed by the aircraft.

5. The method of claim 1, further comprising calculating a near-field effect of the aircraft on a trajectory of the moving object and correcting the flight path of the aircraft for the near-field effect.

6. The method of claim 1, further comprising calculating a near-field effect of the aircraft on a trajectory of the moving object and altering the trajectory of the moving object via the near-field effect.

7. The method of claim 1, wherein the processor determines a reference frame in which the moving object is stationary and maintains the selected offset between the aircraft and the moving object for the determined reference frame and wherein a pilot performs a flight maneuver based on the selected offset.

8. The method of claim 1, wherein the processor wherein the flight maneuver includes changing the offset between the aircraft and the moving object.

9. An autonomous flight control system for an aircraft, comprising:

a perception system at the aircraft for tracking a trajectory of a moving object; and

a processor configured to;

determine, from the trajectory of the moving object, a reference frame in which the moving object is stationary;

establish the aircraft at a selected offset from the moving object for the trajectory of the moving object, and

fly the aircraft along a flight path based on the selected offset using calculations performed with respect to the determined reference frame.

10. The autonomous flight control system of claim 9, wherein the processor is further configured to land one of the aircraft and an item conveyed by the aircraft on the moving object.

11. The autonomous flight control system of claim 9, wherein the processor is further configured to track a rotation of the moving object about an axis and to correct the flight path for the rotation of the moving object.

12. The autonomous flight system of claim 11, wherein the processor is further configured to mimic the rotation of the moving object at one of the aircraft and a slung load conveyed by the aircraft.

13. The autonomous flight system of claim 11, wherein the processor is further configured to calculate a near-field effect of the aircraft on the trajectory of the moving object and correct the flight path of the aircraft for the near-field effect.

14. The autonomous flight system of claim 9, wherein the processor is further configured to calculate a near-field effect of the aircraft on a trajectory of the moving object and alter the trajectory of the moving object via the near-field effect.

15. The autonomous flight system of claim 9, wherein a pilot flies the aircraft to the selected offset between the aircraft and the moving object and the processor is further configured to maintain the selected offset and wherein the pilot is flies the aircraft based on the selected offset.