Ground vehicle-like control for remote control aircraft
US-2015370256-A1 · Dec 24, 2015 · US
US2016004253A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016004253-A1 |
| Application number | US-201514850910-A |
| Country | US |
| Kind code | A1 |
| Filing date | Sep 10, 2015 |
| Priority date | Jan 5, 2011 |
| Publication date | Jan 7, 2016 |
| Grant date | — |
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A self-controlled device maintains a frame of reference about an x-, y- and z-axis. The self-controlled device processes an input to control the self-propelled device, the input being based on the x- and y-axis. The self-propelled device is controlled in its movement, including about each of the x-, y- and z-axis, based on the input.
Opening claim text (preview).
What is claimed is: 1 . A system comprising: a controller device; a self-propelled device including a spherical housing and an internal drive system, the internal drive system being provided within the spherical housing to maneuver the spherical housing under control of the controller device by: maintaining, on the spherical housing, an initial frame of reference that rotates about each of an x-axis, a y-axis, and a z-axis as the spherical housing is maneuvered; receiving, from a two-dimensional steering mechanism of the controller device, two-dimensional control inputs of a user operating a controller device that is external to the spherical housing; implementing the two-dimensional control inputs as three-dimensional, rotational motion about each of the x-axis, the y-axis, and the z-axis, so that the spherical housing is maneuvered about the x-axis, the y-axis, and the z-axis in response to the two-dimensional control inputs being received; and maintaining the initial frame of reference while the spherical housing is maneuvered about the x-axis, the y-axis, and the z-axis. 2 . The system of claim 1 , further comprising: an internal controller that wirelessly receives the two-dimensional inputs. 3 . The system of claim 2 , wherein the internal controller includes a processor. 4 . The system of claim 1 , wherein the initial frame of reference is identifiable by an outwardly visible feature. 5 . A system comprising: a controller device; a self-propelled device including a spherical housing and an internal drive system, the internal drive system being provided within the spherical housing to maneuver the spherical housing under control of the controller device by: maintaining, on the spherical housing, an initial frame of reference that rotates about each of an x-axis, a y-axis, and a z-axis as the spherical housing is maneuvered; receiving, from a two-dimensional steering mechanism of the controller device, two-dimensional control inputs of a user operating a controller device that is external to the spherical housing; implementing the two-dimensional control inputs as three-dimensional, rotational motion about each of the x-axis, the y-axis, and the z-axis, so that the spherical housing is maneuvered about the x-axis, the y-axis, and the z-axis in response to the two-dimensional control inputs being received; and maintaining the initial frame of reference while the spherical housing is maneuvered about the x-axis, the y-axis, and the z-axis; wherein the controller device is calibrated based on the initial frame of reference. 6 . The system of claim 5 , further comprising: an internal controller that wirelessly receives the two-dimensional inputs. 7 . The system of claim 6 , wherein the internal controller includes a processor. 8 . The system of claim 5 , wherein the initial frame of reference is identifiable by an outwardly visible feature. 9 . The system of claim 5 , wherein the controller device executes programmatic instructions to calibrate. 10 . A method for operating a self-propelled device, the method comprising: maintaining, for the self-propelled device, an initial frame of reference that rotates about each of an x-axis, a y-axis, and a z-axis as the self-propelled device moves; receiving, from a two-dimensional steering mechanism of a controller device, a two-dimensional input to control the self-propelled device; translating the two-dimensional input into a three-dimensional, rotational motion of a spherical housing for the self-propelled device, the three-dimensional rotational motion being about each of the x-axis, the y-axis, and the z-axis; and based on translating the two-dimensional input, maneuvering the spherical housing about each of the x-axis, the y-axis, and the z-axis while maintaining the initial frame of reference. 11 . The method of claim 10 , further comprising maneuvering about one or more of the x-axis, the y-axis, or the z-axis, using an internal drive system that is dynamically unstable. 12 . The method of claim 11 , further comprising processing feedback during movement, from one or more sensors of the self-propelled device, to compensate for the internal drive system being dynamically unstable. 13 . The method of claim 12 , wherein processing the feedback includes processing a first input from a three-axis gyroscope sensor of the self-propelled device. 14 . The method of claim 12 , wherein processing the feedback further includes processing a second input from a three-axis accelerometer of the self-propelled device. 15 . The method of claim 14 , wherein the second input is processed by an inertial measurement unit of the self-propelled device to determine the initial frame of reference about each of the x-axis, the y-axis, and the z-axis during when the spherical housing is being maneuvered. 16 . The method of claim 10 , wherein the spherical housing provides a marker to identify the initial frame of reference while the self-propelled device is maneuvered.
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