FIXED-WING DRONE, IN PARTICULAR OF THE FLYING-WING TYPE, WITH ASSISTED MANUAL PILOTING AND AUTOMATIC PILOTING

• US 20180039271A1
• Filed: 08/08/2017
• Published: 02/08/2018
• Est. Priority Date: 08/08/2016
• Status: Abandoned Application

• Current Assignee: Parrot Drones
• Original Assignee: Parrot Drones
• Inventors: RIMOUX, Ariel, PIRAT, Frdric
• Application Number:
  US15/672,246
• Publication Number:
  US 20180039271A1
• Time in Patent Office: Days
• 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 13/18 using automatic pilot
• CPC Class Codes: B64C 39/024 of the remote controlled vehicle type, i.e. RPV
• CPC Class Codes: B64C 39/10 All-wing aircraft
• CPC Class Codes: B64U 10/25 Fixed-wing aircraft VTOL aircraft B64U10/20
• CPC Class Codes: B64U 2101/30 for imaging, photography or videography
• CPC Class Codes: B64U 2201/10 autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
• CPC Class Codes: B64U 2201/20 Remote controls
• CPC Class Codes: B64U 30/20 Rotors; Rotor supports
• CPC Class Codes: B64U 70/60 Take-off or landing of UAVs from a runway using their own power
• CPC Class Codes: G05D 1/0016 characterised by the operator's input device input arrangements for computing systems in general G06F3/00
• CPC Class Codes: G05D 1/0038 by providing the operator with simple or augmented images from one or more cameras located onboard the vehicle, e.g. tele-operation images analyzed by a computer and used for automatic navigation G05D1/0246
• 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 1/042 specially adapted for aircraft
• CPC Class Codes: G05D 1/0653 during a phase of take-off or landing
• CPC Class Codes: G05D 1/0808 specially adapted for aircraft

Abstract

A drone that includes an automatic piloting system that receives internal and/or external piloting instructions, as well as data of instantaneous attitude (φ*, θ*), altitude (z*) and speed (V*) delivered by sensors. Set point calculation circuits calculate, as a function of a model of the aerodynamic behaviour of the drone in flight, roll (φ) and/or pitch (θ) set points and/or speed set points (V) and/or altitude set points (z) corresponding to the internal and/or external piloting instructions received. Correction and control circuits control the propulsion system and the drone control surface servomechanisms. A system further allows generating internally piloting instructions for autonomous flight modes such as automatic take-off or automatic landing.

Claims

1. A fixed-wing drone, comprising:

a propulsion system, control surfaces and an automatic pilot, wherein the automatic pilot is configured to;

calculate set points as a function of instructions, said instructions comprising internal piloting instructions generated by the automatic pilot and external instructions received by the drone, said internal instructions and external instructions comprising turn instructions, move up/move down instructions and speed change instructions, said set points including a roll angle set point (φ

), a pitch angle set point () and a speed set point (V) for the implementation of the internal and/or external instructions; and

control the propulsion system and the control surfaces as a function of the calculated set points,

upon application of a turn instruction and/or a speed change instruction, calculate said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) so as to perform a turn and/or a speed change while maintaining constant an altitude (z) of the drone during the turn and/or the speed change, and

upon cessation of receipt of at least certain of said external piloting instructions generate said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) so as to maintain constant the heading and the altitude the drone had at the time of said cessation of receipt of at least certain of said external piloting instructions.

2. The drone according to claim 1, wherein the automatic pilot is further configured to, upon cessation of receipt of any external piloting instruction, generate said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) so as to further maintain constant the speed the drone had at the time of said cessation of receipt of any external piloting instruction.

3. The drone according to claim 1, wherein said at least certain external piloting instructions comprise the turn external piloting instructions and the move up/move down external piloting instructions, and do not comprise the speed external piloting instructions.

4. The drone according to claim 3, wherein the automatic pilot is further con-figured to, upon receipt of speed external piloting instructions and with no receipt of turn external piloting instructions nor receipt of move up/move down external piloting instructions:

continue generating said roll angle set point (φ

) and said pitch angle set point () so as to maintain constant the heading and the altitude the drone had at the time of said cessation of receipt of turn external piloting instructions and move up/move down external piloting instructions, and

generate said speed set point (V) based on the move up/move down external piloting instructions received.

5. The drone according to claim 3, wherein the automatic pilot is further configured to, upon receipt of turn external piloting instructions or move up/move down external piloting instructions:

stop generating said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) that had been generated so as to maintain constant the heading and the altitude the drone had at the time of said cessation of receipt of turn external piloting instructions and move up/move down external piloting instructions.

6. The drone according to claim 1, wherein, in an autonomous operating mode, the automatic pilot is configured to generate internal piloting instructions including turn instructions, move up/move down instructions and/or speed instructions.

7. The drone according to claim 1, wherein the automatic pilot is configured to generate internal piloting instructions according to an automatic take-off mode with a phase of moving up to a predetermined altitude followed with a phase of waiting in orbital flight at the predetermined altitude.

8. The drone according to claim 7, wherein the automatic take-off mode comprises successively:

a phase of operating the propulsion unit of the propulsion system at slow speed,

a phase of operating the propulsion unit at a faster speed,

a phase of moving up in straight line with holding of the heading, and said phase of waiting in orbital flight when said predetermined altitude is reached.

9. The drone according to claim 1, wherein the automatic pilot is configured to generate internal piloting instructions according to an automatic landing mode, with potential superimposition, onto the piloting instructions generated by the automatic pilot, of external piloting instructions received by the drone.

10. The drone according to claim 9, wherein this automatic landing mode comprises successively:

a phase of moving down to a predetermined altitude,

a phase of moving down along a helical trajectory or according to a linear trajectory, and

a phase of inversion of the direction of rotation of the propulsion unit of the propulsion system.

11. The drone according to claim 1, wherein the automatic pilot is configured to calculate the set points as a function of a difference between the air speed of the drone and the ground speed of the drone.

12. The drone according to claim 1, wherein the automatic pilot is configured to calculate the set points so as to fly at constant air speed or at constant ground speed in a constant-speed operating mode.

13. The drone according to claim 1, wherein, for the execution of a turn instruction, the automatic pilot is configured to calculate the set points so as to perform the turn with a constant turn rate with respect to the ground.

14. A method of piloting a fixed-wing drone comprising a propulsion system, control surfaces and an automatic pilot, the method comprising the steps of:

calculating set points as a function of piloting instructions comprising internal instructions, generated by the automatic pilot, and/or external instructions, received by the drone, said internal instructions and external instructions comprising turn instructions, move up/move down instructions and speed change instructions, said set points including a roll angle set point (φ

), a pitch angle set point () and a speed set point (V) for the implementation of the internal and/or external instructions;

upon application of a turn instruction and/or a speed change instruction, calculating said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) so as to perform a turn and/or a speed change while maintaining constant an altitude (z) of the drone during the turn and/or the speed change;

controlling the propulsion system and the control surfaces as a function of the calculated set points; and

upon cessation of receipt of at least certain of said external piloting instructions, generating said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) so as to maintain constant the heading and the altitude the drone had at the time of said cessation of receipt of at least certain of said external piloting instructions.

15. The method according to claim 14, wherein, upon cessation of receipt of any external piloting instruction, said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) are generated so as to further maintain constant the speed the drone had at the time of said cessation of receipt of any external piloting instruction.

16. The method according to claim 14, wherein said at least certain external piloting instructions comprise the turn external piloting instructions and the move up/move down external piloting instructions, and do not comprise the speed external piloting instructions.

17. The method according to claim 16, further comprising, upon receipt of speed external piloting instructions and with no receipt of turn external piloting instructions nor receipt of move up/move down external piloting instructions, continuing generating said roll angle set point (φ

) and said pitch angle set point (□

) so as to maintain constant the heading and the altitude the drone had at the time of said cessation of receipt of turn external piloting instructions and move up/move down external piloting instructions, and generating said speed set point (V) based on the move up/move down external piloting instructions received.

18. The method according to claim 16, further comprising, upon receipt of turn external piloting instructions or move up/move down external piloting instructions, stopping generating said roll angle set point (φ

), said pitch angle set point () and said speed set point (V) that had been generated so as to maintain constant the heading and the altitude the drone had at the time of said cessation of receipt of turn external piloting instructions and move up/move down external piloting instructions