Systems and methods for adjusting uav trajectory

US2018362158A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2018362158-A1
Application numberUS-201816109991-A
CountryUS
Kind codeA1
Filing dateAug 23, 2018
Priority dateFeb 26, 2016
Publication dateDec 20, 2018
Grant date

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A system for controlling an unmanned aerial vehicle (UAV) includes a first user interface configured to receive a first user input and a second user interface configured to receive a second user input. The first user input provides one or more instructions to effect an autonomous flight of the UAV. The second user input provides one or more instructions to modify the autonomous flight of the UAV, The autonomous flight includes a flight towards a target.

First claim

Opening claim text (preview).

What is claimed is: 1 . A system for controlling an unmanned aerial vehicle (UAV), comprising: a first user interface configured to receive a first user input, the first user input providing one or more instructions to effect an autonomous flight of the UAV; and a second user interface configured to receive a second user input, the second user input providing one or more instructions to modify the autonomous flight of the UAV; wherein the autonomous flight includes a flight towards a target. 2 . The system of claim 1 , wherein the target includes a target object or a target destination. 3 . The system of claim 1 , wherein the autonomous flight includes at least one of: a flight to a predetermined location; an autonomous return of the UAV; an autonomous navigation along one or more waypoints; an autonomous flight to a point of interest; a flight along a preset trajectory or a preset direction; a flight along an autonomously planned trajectory; a flight along a user configured trajectory; a flight to a tapped location on a map of the first user interface; or a flight tracking a target object. 4 . The system of claim 1 , wherein the first user interface is located on a first device and the second user interface is located on a second device. 5 . The system of claim 4 , wherein: the first device or the second device includes a handheld device or a mobile device, the handheld or mobile device including a cell phone, tablet, or PDA; and the second device includes a remote controller. 6 . The system of claim 4 , wherein the first device and the second device are operably coupled to one another. 7 . The system of claim 1 , wherein the first user interface and the second user interface are located on a single device. 8 . The system of claim 1 , wherein: the first user interface includes a touch screen; and the first user input is received via a user tapping on the touch screen. 9 . The system of claim 1 , wherein the first user interface is configured to show a location of the UAV on a two dimensional map and/or display images received from a camera coupled to the UAV. 10 . The system of claim 1 , wherein the second user interface includes one or more actuatable mechanisms, the one or more mechanisms including one or more control sticks. 11 . The system of claim 11 , wherein: the one or more control sticks include at least one of a roll stick configured to affect a rotation of the UAV about a roll axis and a yaw stick configured to affect a rotation of the UAV about a yaw axis. 12 . The system of claim 11 , wherein an actuation of the one or more control sticks is configured to effect at least one of: adding a direction component along a horizontal plane and perpendicular to an autonomous flight path of the UAV, a degree of the actuation corresponding to a magnitude of the direction component; adding a velocity component along the horizontal plane and perpendicular to the autonomous flight path of the UAV, a degree of the actuation corresponding to a magnitude of the velocity component; adding an acceleration component to the autonomous flight path of the UAV, a degree of the actuation corresponding to a magnitude of the acceleration component; adding a centripetal acceleration to the UAV, a degree of the actuation inversely corresponding to a size of a radius of a trajectory arc of the UAV. 13 . The system of claim 11 , wherein the one or more control sticks is configured to stop the autonomous flight. 14 . The system of claim 1 , wherein the first user interface is further configured to display at least one of an autonomous flight path of the UAV or a modified flight path of the UAV. 15 . The system of claim 1 , wherein the second user input is configured to modify the autonomous flight of the UAV for a duration of the second user input, including modifying at least one of an altitude of the UAV, a trajectory of the UAV, a velocity of the UAV, or an acceleration of the UAV. 16 . The system of claim 1 , wherein the autonomous flight of the UAV is modified further taking into account environmental factors in concert with the second user input, the environmental factors being determined based on one or more sensors on board the UAV, the one or more sensors including a camera. 17 . The system of claim 1 , wherein the autonomous flight of the UAV is modified by a flight controller that takes into account the second user input. 18 . The system of claim 1 , wherein after the second user input is received and released, the UAV is configured to: fly along a prior flight path it was flying along prior to receiving the one or more instructions to modify the autonomous flight of the UAV; or fly along a new flight path different from the prior flight path. 19 . A method of controlling an unmanned aerial vehicle (UAV), comprising: receiving a first user input at a first user interface, the first user input providing one or more instructions to effect an autonomous flight of the UAV; and receiving a second user input at a second user interface, the second user input providing one or more instructions to modify the autonomous flight of the UAV; wherein the autonomous flight includes a flight towards a target. 20 . A non-transitory computer readable medium storing code, logic, or instructions to: receive a first user input at a first user interface, the first user input providing one or more instructions to effect an autonomous flight of an unmanned aerial vehicle (UAV); and receive a second user input at a second user interface, the second user input providing one or more instructions to modify the autonomous flight of the UAV; wherein the autonomous flight includes a flight towards a target.

Assignees

Inventors

Classifications

  • Remote controls · CPC title

  • autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS] · CPC title

  • characterised by the operator's input device (input arrangements for computing systems in general G06F3/00) · CPC title

  • Physics · mapped topic

  • characterized by the autonomous decision making process, e.g. artificial intelligence, predefined behaviours (using knowledge based models G06N5/00) · CPC title

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What does patent US2018362158A1 cover?
A system for controlling an unmanned aerial vehicle (UAV) includes a first user interface configured to receive a first user input and a second user interface configured to receive a second user input. The first user input provides one or more instructions to effect an autonomous flight of the UAV. The second user input provides one or more instructions to modify the autonomous flight of the UA…
Who is the assignee on this patent?
Sz Dji Technology Co Ltd
What technology area does this patent fall under?
Primary CPC classification B64C39/024. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Dec 20 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 4 related publications on this page (citations in our corpus or others sharing the same primary CPC).