# US 12,216,479 B2 · Methods for launching and landing an unmanned aerial vehicle

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- Number: US 12,216,479 B2
- Document ID: US12216479B2
- Status: Granted
- Kind: B2
- Application number: 18/449,447
- Filed: 2023-08-14
- Published: 2023-12-21
- Granted: 2025-02-04
- Earliest claimed: 2017-05-30
- Assignees: Sz Dji Technology Co., Ltd.
- Applicants: Sz Dji Technology Co., Ltd.
- Inventors: Mingyu Wang
- Web page: https://patentgrep.com/patent/US12216479B2

## CPC

- G05D 1/0669: {specially adapted for vertical take-off}
- A63H 27/12: {Helicopters (A63H27/04 takes precedence); Flying tops}
- B64U 10/10: Rotorcrafts
- B64U 10/14: with four distinct rotor axes, e.g. quadcopters
- B64U 20/80: Arrangement of on-board electronics, e.g. avionics systems or wiring
- B64U 50/00: Propulsion; Power supply
- B64U 60/20: specially adapted for uneven terrain
- B64U 70/10: for releasing or capturing UAVs by hand
- B64U 70/95: Means for guiding the landing UAV towards the platform, e.g. lighting means
- B64U 80/30: with arrangements for data transmission
- G05D 1/0011: {associated with a remote control arrangement}
- G05D 1/0676: {specially adapted for landing}
- G05D 1/223: Command input arrangements on the remote controller, e.g. joysticks or touch screens
- G05D 1/652: Take-off (delivering or retrieving payloads G05D1/667)
- G05D 1/654: Landing (docking at a base station G05D1/661)
- B64U 2101/30: for imaging, photography or videography
- B64U 2101/60: for transporting passengers; for transporting goods other than weapons
- B64U 2201/10: autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
- B64U 2201/20: Remote controls
- G05D: SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- A63H: TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- B64U: UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR

## Abstract

An aerial vehicle landing method includes controlling to decelerate, with aid of one or more processors and in response to at least two of a plurality of conditions being satisfied, the aerial vehicle to cause the aerial vehicle to land autonomously. The plurality of conditions includes determining that an external signal related to a human is detected via one or more sensors; determining that a location/orientation change of the aerial vehicle is detected while the aerial vehicle is airborne; and determining that an external contact from an external object is exerted upon the aerial vehicle, the external object being an object that is not part of the aerial vehicle.

## Claims

### Claim 1

An aerial vehicle landing method comprising:
controlling to decelerate, with aid of one or more processors and in response to at least two of a plurality of conditions being satisfied, an aerial vehicle to cause the aerial vehicle to land autonomously, the plurality of conditions including:
determining that an external signal related to a human is detected via one or more sensors;
determining that a location/orientation change of the aerial vehicle is detected while the aerial vehicle is airborne; and
determining that an external contact from an external object is exerted upon the aerial vehicle, the external object being an object that is not part of the aerial vehicle.

### Claim 2 (depends on 1)

The landing method of claim 1, wherein the external signal includes at least one of a visual signal or an audio signal of the human.

### Claim 3 (depends on 2)

The landing method of claim 2, wherein the visual signal includes a gesture, a movement, or an image of the human.

### Claim 4 (depends on 3)

The landing method of claim 3, wherein the gesture or movement of the human includes a gesture, a movement, or an image of at least one of a hand, arm, head, facial feature, or eyes of the human.

### Claim 5 (depends on 3)

The landing method of claim 3, wherein the gesture or movement of the human includes at least one of a wave of a hand or arm of the human, a turn of a head of the human, or a movement of an eye of the human.

### Claim 6 (depends on 1)

The landing method of claim 1, wherein the one or more sensors includes at least one of a visual sensor, an audio sensor, an altimeter, a proximity sensor, or a motion detector.

### Claim 7 (depends on 1)

The landing method of claim 1, wherein controlling to decelerate the aerial vehicle to cause the aerial vehicle to land autonomously includes:
receiving a deceleration signal from a controller of the aerial vehicle, the controller being configured to generate the deceleration signal in response to the at least two of a plurality of conditions being satisfied; and
controlling to decelerate, in response to the deceleration signal being received, the aerial vehicle to cause the aerial vehicle to land autonomously.

### Claim 8 (depends on 1)

The landing method of claim 1, wherein controlling to decelerate the aerial vehicle to cause the aerial vehicle to land autonomously includes:
controlling the aerial vehicle to land at a designated location.

### Claim 9 (depends on 1)

The landing method of claim 1, wherein controlling to decelerate the aerial vehicle to cause the aerial vehicle to land autonomously includes:
controlling to bring the aerial vehicle to a stop in response to determining a contact of the aerial vehicle with a landing surface.

### Claim 10 (depends on 9)

The landing method of claim 9, wherein:
the landing surface includes a human hand; and
controlling to bring the aerial vehicle to the stop in response to determining the contact of the aerial vehicle with the landing surface:
controlling to bring the aerial vehicle to the stop in response to determining the contact of the aerial vehicle with the human hand.

### Claim 11 (depends on 1)

The landing method of claim 1, wherein the aerial vehicle is a rotorcraft including one or more rotor blades, and wherein controlling to decelerate the aerial vehicle includes causing the one or more rotor blades to slow down, stall, or come to a complete stop.

### Claim 12 (depends on 11)

The landing method of claim 11, wherein the one or more processors are further configured to:
stopping rotation of the one or more rotor blades of the aerial vehicle in response to the external contact of the aerial vehicle after the external contact is sustained for a predetermined time period.

### Claim 13 (depends on 1)

The landing method of claim 1, wherein the location/orientation change of the aerial vehicle while the aerial vehicle is airborne includes the location/orientation change of the aerial vehicle while the aerial vehicle is hovering near or is passing by a person.

### Claim 14 (depends on 1)

The landing method of claim 1, wherein the location/orientation change of the aerial vehicle includes a change of a location of the aerial vehicle with respect to a frame of reference or a reference object.

### Claim 15 (depends on 1)

The landing method of claim 1, wherein the location/orientation change of the aerial vehicle includes at least one of a change of a velocity, a change of an acceleration, a change of an orientation, or a change of a location of the aerial vehicle.

### Claim 16 (depends on 1)

The landing method of claim 1, further comprising:
detecting the external contact via at least one of a touch sensor, a temperature sensor, a pressure sensor, an altimeter, a proximity sensor, or a photo sensor.

### Claim 17

An aerial vehicle, comprising:
one or more processors configured to control to decelerate, in response to at least two of a plurality of conditions being satisfied, the aerial vehicle to cause the aerial vehicle to land autonomously, the plurality of conditions including:
determining that an external signal related to a human is detected via one or more sensors;
determining that a location/orientation change of the aerial vehicle is detected while the aerial vehicle is airborne; and
determining that an external contact from an external object is exerted upon the aerial vehicle, the external object being an object that is not part of the aerial vehicle.

### Claim 18 (depends on 17)

The aerial vehicle of claim 17, wherein the one or more processors are further configured to:
controlling to bring the aerial vehicle to a stop in response to detecting a contact of the aerial vehicle with a landing surface, the landing surface includes a human hand.

### Claim 19

An aerial vehicle, comprising:
one or more processors configured to, in response to detecting, by one or more sensors, an external signal related to a human or a change of a location/orientation of the aerial vehicle caused by the human holding and moving the aerial vehicle:
control the aerial vehicle to land on a hand of the human; or
control the aerial vehicle to generate a lift and/or thrust, to launch from the hand of the human.

### Claim 20 (depends on 19)

The aerial vehicle of claim 19, wherein the external signal includes a gesture, a movement, or an image of the human.
