초록 ▼

Launch-controlled unmanned aerial vehicles, and associated systems and methods are disclosed. A computer-implemented method for operating an unmanned aerial vehicle in a representative embodiment includes detecting at least one parameter of a motion of the UAV as a user releases the UAV for flight.

Launch-controlled unmanned aerial vehicles, and associated systems and methods are disclosed. A computer-implemented method for operating an unmanned aerial vehicle in a representative embodiment includes detecting at least one parameter of a motion of the UAV as a user releases the UAV for flight. Based at least in part on the at least the one detected parameter, the method can further include establishing a flight path for the UAV, and directing the UAV to fly the flight path.

대표청구항 ▼

1. A computer-implemented method for operating an unmanned aerial vehicle (UAV), comprising: detecting at least one parameter of a motion of the UAV as a user releases the UAV for flight;projecting a vector of the release on a surface based at least on the detected at least one parameter;establishin

1. A computer-implemented method for operating an unmanned aerial vehicle (UAV), comprising: detecting at least one parameter of a motion of the UAV as a user releases the UAV for flight;projecting a vector of the release on a surface based at least on the detected at least one parameter;establishing a flight path for the UAV based at least on one of the projected vector or a position on the surface corresponding to the projected vector; anddirecting the UAV to fly the flight path. 2. The method of claim 1 wherein the flight path includes a target location, and wherein the flight path is the only flight path used by the UAV to reach the target location. 3. The method of claim 1 wherein detecting at least one parameter includes detecting an acceleration. 4. The method of claim 1 wherein detecting at least one parameter includes detecting a direction. 5. The method of claim 1 wherein detecting the at least one parameter includes detecting an acceleration and a direction, and wherein the acceleration is correlated with a target distance on the flight path, and wherein the direction is correlated with a direction of the flight path. 6. The method of claim 1 further comprising: determining the flight path, including determining a target orientation of the UAV at a target location on the flight path, wherein the target orientation includes an orientation in which the UAV is facing a user. 7. The method of claim 1 wherein the motion includes a release from the user's hand during launch. 8. The method of claim 1, wherein the surface is a flat surface. 9. The method of claim 1 wherein the flight path includes a first segment in a direction away from the user and a second segment back to the user, with both the first and second segments executed autonomously without external input after the user releases the UAV for flight. 10. The method of claim 1 wherein the flight path includes a first segment in a direction away from the user and a second segment back to the user, and wherein the method further comprises: in response to sensing the user catching the UAV, automatically turning off propellers carried by the UAV. 11. The method of claim 10, further comprising sensing the user catching the UAV, and wherein the sensing includes sensing an acceleration. 12. The method of claim 1 wherein the flight path includes a segment in a direction away from the user, and wherein the method further comprises directing the UAV to turn toward the user based on the direction of the segment. 13. The UAV of claim 12, further comprising directing the UAV to capture an image of the user when turned toward the user. 14. A propulsion system for an unmanned aerial vehicle (UAV) that includes a flyable support structure that caries the propulsion system, the system comprising: a power source;at least one propeller; anda sensor carried by the support structure and coupled to the power source, the sensor being configured to detect at least one parameter of a motion of the UAV as a user releases the UAV for flight, wherein the at least one parameter of the motion includes a direction of motion of the UAV as the user releases the UAV; anda controller operatively coupled to the sensor and programed with instructions that, when executed, perform actions including:receive an indication of the at least one parameter;based at least in part on the at least one parameter, establish a flight path for the UAV that includes a target location and establish a direction to the target location based at least in part on the direction of motion of the UAV as the user releases the UAV; anddirect the UAV to fly the flight path. 15. The system of claim 14 wherein the flight path is the only flight path used by the UAV to reach the target location. 16. The system of claim 14 wherein the flyable support structure is a wearable support structure. 17. The system of claim 14 wherein the sensor includes an accelerometer. 18. The system of claim 17, the actions further include: employ the accelerometer to determine one or more accelerations of the UAV;when at least one of the one or more accelerations is less than a first acceleration threshold, detect a freefall event and initiate operating the power source; andwhen the at least one of the one or more accelerations is greater than a second acceleration threshold, detect a catch event and terminate operating the power source. 19. The system of claim 14 wherein the UAV includes a camera and the actions further include: automatically orient the camera toward the user. 20. The system of claim 14 wherein the at least one parameter of motion further includes an absolute value of a throw velocity vector and the direction of motion of the UAV includes a first angle of the throw velocity vector and a second angle of the throw velocity vector, and the actions further include: determine a turning point of the UAV based on each of the absolute value of the throw velocity angle, the first angle of the throw velocity vector, and the second angle of the throw velocity vector. 21. A method for manufacturing an unmanned aerial vehicle (UAV), comprising: programming a controller of the UAV with instructions, that, when executed, perform actions comprising: detect at least one parameter of a motion of the UAV as a user releases the UAV for flight, wherein the at least one parameter includes an acceleration of the UAV;based at least in part on the detected at least one parameter, establish a flight path for the UAV that includes a target location and establish a distance to the target location that is correlated with the acceleration of the UAV; anddirect the UAV to fly the flight path. 22. The method of claim 21 wherein detecting at least one parameter includes detecting a direction of the UAV at release, and wherein establishing a flight path includes establishing a direction to the target location based at least in part on the direction of the UAV at release. 23. The method of claim 21 wherein establishing the flight path includes projecting a vector of the release onto a surface. 24. The method of claim 21 wherein the at least one parameter further includes an axis of a spin of the UAV provided by the user and the flight path is further based on a surface that corresponds to the axis of the spin. 25. The method of claim 21 the actions further comprising: employ an inductance sensor to detect the user releasing the UAV for flight; andin response to detecting the user releasing the UAV for flight, initiate flight operations of the UAV. 26. The method of claim 21 the actions further comprising: prior to the user releasing the UAV, detect a swinging gesture of the user; andin response to detecting the swinging gesture of the user, establish the flight path to further include a circle around the user.