IP Library Granted Patent US 12,468,298
Granted Patent B2
US 12,468,298 · App. 18/629,029 · Granted Nov 11, 2025

Safety system for operation of an unmanned aerial vehicle

Inventors: Thaddeus Benjamin Matuszeski (Pasadena, CA); William Arden Lott (Simi Valley, CA); Derek Lisoski (Simi Valley, CA)
Assignee: AeroVironment, Inc.
G05D1/0055B64C39/024B64U10/20G05D1/0016G05D1/223G05D1/617B64U10/10B64U10/25B64U30/10B64U30/20B64U70/00B64U70/80B64U80/25B64U80/30B64U2101/30B64U2201/10B64U2201/20H04N7/185
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 12,468,298
App. No.
18/629,029
Granted
Nov 11, 2025
Kind
B2
Abstract

Systems, devices, and methods for a safety system including: selecting an unmanned aerial vehicle (UAV) command on a controller, the controller comprising a first processor with addressable memory; presenting a first activator and a second activator on a display of the controller for the selected UAV command, wherein the second activator is a slider; and sending the UAV command to a UAV if the first activator and the second activator are selected, the UAV comprising a second processor with addressable memory.

Claims (31)

1 . A system for operation of an unmanned aerial vehicle (UAV) comprising:

a controller having a first processor and a first addressable memory, wherein the controller is configured to:

present a first activator and a second activator on a display screen of the controller, wherein the first activator is presented as a first user interface (UI) element comprising a button and the second activator is presented as a second UI element comprising a slider;

select the first activator and the second activator, wherein the selection of the second activator is subsequent to the selection of the first activator; and

transmit a UAV command to control the UAV via a transmitter of the controller based on the selection of the first activator and the second activator.

2 . The system of claim 1 , wherein the UAV comprises a second processor with a second addressable memory and a receiver configured to receive the transmitted UAV command.

3 . The system of claim 2 further comprising:

the UAV having the second processor and addressable memory, the second processor configured to:

receive the transmitted UAV command; and

execute the received UAV command on the UAV.

4 . The system of claim 1 , wherein the transmitted UAV command is based on a direction of movement of the button in the slider of the second activator.

5 . The system of claim 4 , wherein the direction of movement corresponds to an action of the UAV.

6 . The system of claim 1 , wherein the transmitted UAV command is selected on the controller prior to presenting the first activator and the second activator on the display screen.

7 . The system of claim 1 , wherein the UAV command is transmitted based on the selection of the first activator being maintained while the second activator is selected.

8 . The system of claim 1 , wherein the transmitted UAV command is a launch command, wherein the second activator is a vertical slider, and wherein selecting the second activator comprises sliding the button in an upward direction in the slider relative to a display screen of the controller.

9 . The system of claim 1 , wherein the transmitted UAV command is a return and land command, wherein the second activator is a horizontal slider, and wherein selecting the second activator comprises sliding the button horizontally in the slider relative to a display screen of the controller.

10 . The system of claim 9 , wherein the return and land command directs the UAV to land at a location it launched from.

11 . The system of claim 1 , wherein the transmitted UAV command is a land now command, wherein the second activator is a vertical slider, and wherein selecting the second activator comprises sliding the button in a downward direction in the slider relative to a display screen of the controller.

12 . The system of claim 11 , wherein the land now command directs the UAV to land at a location proximate to a geographical position of the UAV when the UAV receives the land now command.

13 . The system of claim 1 , wherein the transmitted UAV command is an emergency stop command, wherein the second activator is a vertical slider, and wherein selecting the second activator comprises sliding the button in a downward direction in the slider relative to a display screen of the controller.

14 . The system of claim 13 , wherein the emergency stop command directs the UAV to stop at least one motor of the UAV.

15 . A method for operation of an unmanned aerial vehicle (UAV) comprising:

presenting a first activator and a second activator on a display screen of a controller, the controller comprising a first processor with a first addressable memory, wherein the first activator is presented as a first user interface (UI) element comprising a button, and wherein the second activator is presented as a second UI element comprising a slider;

selecting the first activator and the second activator, wherein the selection of the second activator is subsequent to the selection of the first activator; and

transmitting a UAV command to control the UAV via a transmitter of the controller based on the selection of the first activator and the second activator at least one of: simultaneously and sequentially with the second activator.

16 . The method of claim 15 , wherein the UAV comprises a second processor with a second addressable memory and a receiver configured to receive the transmitted command.

17 . The method of claim 15 , wherein the transmitted UAV command is a wireless signal.

18 . The method of claim 15 , wherein the transmitted UAV command is based on a direction of movement of the button in the slider of the second activator.

19 . The method of claim 15 , further comprising, prior to transmitting the UAV command:

generating the UAV command for the UAV on the controller based on the direction of movement of the button in the slider of the second activator.

20 . The method of claim 19 , wherein the direction of movement corresponds to an action of the UAV.

Assignments (2)
SECURITY INTEREST Recorded Oct 4, 2024
From: AEROVIRONMENT, INC.
To: BANK OF AMERICA, N.A., AS THE ADMINISTRATIVE AGENT
Reel/Frame 069113/0683 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 15, 2024
From: MATUSZESKI, THADDEUS BENJAMIN; LOTT, WILLIAM ARDEN; LISOSKI, DEREK
To: AEROVIRONMENT, INC.
Reel/Frame 067107/0711 →
Continuity (5)
Continuation 17316100 · May 10, 2021
Continuation 16241341 · Jan 7, 2019
Continuation 15808783 · Nov 9, 2017
Provisional Application 62421163 · Nov 11, 2016
Related Publication 20240255945A1 · Aug 1, 2024
References Cited (59)
US 9033281B1 · Adams · 2015 [cited by examiner]
US 9164506B1 · Zang · 2015 [cited by applicant]
US 9412278B1 · Gong et al. · 2016 [cited by applicant]
US 10209707B2 · Matuszeski · 2019 [cited by examiner]
US 11029684B2 · Matuszeski · 2021 [cited by examiner]
US 20040001105A1 · Chew et al. · 2004 [cited by applicant]
US 20060224280A1 · Flanigan et al. · 2006 [cited by applicant]
US 20070150842A1 · Chaudhri et al. · 2007 [cited by applicant]
US 20080114603A1 · Desrochers · 2008 [cited by applicant]
US 20100084513A1 · Gariepy et al. · 2010 [cited by applicant]
US 20100305778A1 · Dorneich et al. · 2010 [cited by applicant]
US 20110014983A1 · Miller · 2011 [cited by applicant]
US 20110288696A1 · Lefebure · 2011 [cited by applicant]
US 20120191269A1 · Chen et al. · 2012 [cited by applicant]
US 20120280087A1 · Coffman et al. · 2012 [cited by applicant]
US 20140217874A1 · Lin et al. · 2014 [cited by applicant]
US 20140249693A1 · Stark et al. · 2014 [cited by applicant]
US 20150158392A1 · Zhao · 2015 [cited by applicant]
US 20150321758A1 · Sarna · 2015 [cited by applicant]
US 20150344136A1 · Dahlstrom · 2015 [cited by applicant]
US 20150346722A1 · Herz et al. · 2015 [cited by applicant]
US 20150362917A1 · Wang et al. · 2015 [cited by applicant]
US 20160023755A1 · Elshafei et al. · 2016 [cited by applicant]
US 20160062539A1 · Moon et al. · 2016 [cited by applicant]
US 20160165290A1 · Szarek et al. · 2016 [cited by applicant]
US 20160280370A1 · Canavor et al. · 2016 [cited by applicant]
US 20160285864A1 · Canavor et al. · 2016 [cited by applicant]
US 20160306351A1 · Fisher et al. · 2016 [cited by applicant]
US 20160321503A1 · Zhou · 2016 [cited by applicant]
US 20160371987A1 · Kotecha · 2016 [cited by examiner]
US 20160376004A1 · Claridge et al. · 2016 [cited by applicant]
US 20170061813A1 · Tao et al. · 2017 [cited by applicant]
US 20170154536A1 · Kreiner et al. · 2017 [cited by applicant]
US 20170233071A1 · Pilskalns et al. · 2017 [cited by applicant]
US 20170269594A1 · Sydnor · 2017 [cited by applicant]
US 20170277176A1 · Hutson · 2017 [cited by applicant]
US 20180068567A1 · Gong et al. · 2018 [cited by applicant]
US 20180079530A1 · Wyrobek · 2018 [cited by applicant]
US 20180143627A1 · Lee et al. · 2018 [cited by applicant]
US 20180321676A1 · Matuszeski · 2018 [cited by examiner]
US 20190138001A1 · Matuszeski et al. · 2019 [cited by applicant]
CN 101983368A · 2011 [cited by applicant]
CN 103592948A · 2014 [cited by applicant]
CN 103869255A · 2014 [cited by applicant]
CN 104267738A · 2015 [cited by applicant]
CN 104349875A · 2015 [cited by applicant]
CN 104903803A · 2015 [cited by applicant]
CN 105000170A · 2015 [cited by applicant]
CN 105425952A · 2016 [cited by applicant]
CN 205120933U · 2016 [cited by applicant]
CN 105549604A · 2016 [cited by applicant]
CN 105739533A · 2016 [cited by applicant]
CN 105759218A · 2016 [cited by applicant]
CN 105843241A · 2016 [cited by applicant]
CN 104685445B · 2018 [cited by applicant]
FR 2938774A1 · 2010 [cited by applicant]
KR 1020160080253A · 2016 [cited by applicant]
WO 2016050099A1 · 2016 [cited by applicant]
International Search Report for PCT Serial No. PCT/US2017/060945 mailed Mar. 29, 2018. [cited by applicant]