METHOD OF PILOTING A MULTIPLE ROTOR ROTARY-WING DRONE TO FOLLOW A CURVILINEAR TURN

• US 20120232718A1
• Filed: 03/01/2012
• Published: 09/13/2012
• Est. Priority Date: 03/08/2011
• Status: Active Grant

• Current Assignee: Parrot Drones
• Original Assignee: Parrot SA
• Inventors: Rischmuller, Michael, D'haeyer, Frederic
• Granted Patent: US 8,473,125 B2
• Time in Patent Office: Days
• US Class Current: 701/2
• CPC Class Codes: A63H 27/12 Helicopters A63H27/04 takes precedence; Flying tops
• CPC Class Codes: A63H 30/04 using wireless transmission
• CPC Class Codes: B64C 2203/00 Flying model aircraft, flying toy aircraft
• CPC Class Codes: B64U 10/13 Flying platforms
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 50/19 using electrically powered motors
• CPC Class Codes: B64U 70/80 Vertical take-off or landing, e.g. using rockets rotorcrafts B64U10/10; VTOL aircraft B64U10/20
• CPC Class Codes: G05D 1/0202 specially adapted to aircraft
• CPC Class Codes: G08C 17/02 using a radio link
• CPC Class Codes: G08C 2201/93 Remote control using other portable devices, e.g. mobile phone, PDA, laptop

Abstract

The respective motors of the drone (10) can be controlled to rotate at different speeds in order to pilot the drone both in attitude and speed. A remote control appliance produces a command to turn along a curvilinear path, this command comprising a left or right turning direction parameter and a parameter that defines the radius of curvature of the turn. The drone receives said command and acquires instantaneous measurements of linear velocity components, of angles of inclination, and of angular speeds of the drone. On the basis of the received command and the acquired measurements, setpoint values are generated for a control loop for controlling motors of the drone, these setpoint values controlling horizontal linear speed and inclination of the drone relative to a frame of reference associated with the ground so as to cause the drone to follow curvilinear path (C) at predetermined tangential speed (u).

Claims

1. A method of piloting a rotary wing drone (10), the method comprising the following steps:

a) a remote control appliance (16) producing a turning command to follow a curvilinear path;

b) the drone both i) receiving said command and ii) acquiring instantaneous measurements of the linear velocity components, of the angles of inclination, and of the angular velocities of the drone; and

c) on the basis of the received command and of the measurements acquired in step b), generating setpoint values for a drone control loop (64-80), these setpoint values controlling the horizontal linear speed and the inclination of the drone relative to a frame of reference associated with the ground so as to make the drone follow said curvilinear path (C) with a predetermined tangential speed (u), wherein;

the drone is a drone of the quadricopter type having multiple rotors driven by respective motors (72);

the control loop (64-80) controls the horizontal linear speed and the inclination of the drone by taking different actions on the speeds of rotation of said motors (72); and

said command is a rate of turn command comprising a right or left turn direction parameter and a parameter defining a setpoint for the instantaneous radius of curvature of the turn.

2. The method of claim 1, wherein said curvilinear path (C) is a circular path, followed with a constant radius of curvature (R).

3. The method of claim 1, wherein said predetermined tangential speed (u) is a constant speed.

4. The method of claim 1, wherein the setpoint values generated in step c) control the motors of the drone in such a manner as to ensure that the altitude of the drone is also kept constant relative to the ground.

5. The method of claim 1, wherein the setpoint values generated in step c) control the horizontal linear speed and the inclination of the drone in such a manner as to also maintain the drone at a zero radial speed (v) relative to the circular path, so as to compensate for any side-slip or oversteer of the drone as it follows said path.

6. The method of claim 1, wherein, in step a), the command for turning along a curvilinear path is produced by said remote control appliance (16), which appliance comprises:

a touch screen (18);

means suitable for i) detecting contact of at least one digit (20) of a user on the surface of the screen, ii) determining the position of the point(s) of contact, and iii) producing corresponding piloting commands including said command to turn along a curvilinear path; and

wireless data transmission means suitable for transmitting commands to the drone.

7. The method of claim 6, wherein the command to turn along a curvilinear path is triggered on detecting simultaneous contact of two of the user'"'"'s digits on the touch screen.

8. The method of claim 7, wherein said command to turn along a curvilinear path is produced throughout the duration of said simultaneous contact of two digits, and until loss of this simultaneous contact is detected.

9. The method of claim 6, wherein the remote control appliance further includes a detector of inclinations about one and/or both of its pitching and/or roll axes (32, 34), and the command for turning along a curvilinear path is produced i) as a function of the left or right direction of the inclination of the appliance relative to its roll axis (34) in order to determine said left or right turn direction parameter, and ii) as a function of the amplitude of the inclination of the appliance relative to said roll axis (34) in order to determine said parameter defining the radius of curvature (R) of the turn.

10. The method of claim 9, wherein the turn command is also produced as a function of the amplitude of the inclination of the appliance relative to its pitching axis (32), in order to determine a tangential speed parameter (u).

11. The method of claim 1, wherein, if the path followed during a command to turn along a curvilinear path includes a radial velocity component (v), then the turn command is also produced as a function of the amplitude of the inclination of the drone relative to its pitching axis so as to cancel said radial velocity component.

12. The method of claim 1, further including, where appropriate, limiting the radius of curvature (R) of the path to a predetermined minimum value.

13. The method of claim 1, further including, in step a), producing an about-turn command for the drone, and in step c), the travel of the drone along the curvilinear path is ended when the measurements acquired in step b) indicate that the drone has turned through 180°

about its yaw axis.

14. Software, downloadable in part into a digital memory of a rotary wing drone and impart into a digital memory of a remote control appliance, the software including instructions that, on being executed, implement a method according to claim 1 for piloting the drone to turn along a curvilinear path.