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公开(公告)号:US11572259B2
公开(公告)日:2023-02-07
申请号:US16897961
申请日:2020-06-10
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev , Vadim Zlotnik , Alexander Maryanovsky , Roman Dvorkin
Abstract: A method for passive aerial cord release mechanisms and an aerial cord release mechanism for an aerial vehicle (AV). A method includes determining a retracting force to be applied to a winch of an aerial vehicle (AV), wherein the determined retracting force is a force required to retract a cord to be coiled around the winch within the AV, and the cord is temporarily coupled to the winch, such that an external force exceeding a predetermined threshold causes decoupling between the cord and the winch.
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公开(公告)号:US12211390B2
公开(公告)日:2025-01-28
申请号:US17510812
申请日:2021-10-26
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev , Ophir Marko
IPC: G08G5/00 , G05D1/00 , B64U101/64
Abstract: A method and system for optimizing drone delivery efficiency. The method includes determining an optimal intermediate location for a UAV based on historical payload delivery data related to a payload carried by the UAV, wherein the distance between the optimal intermediate location and each of a group of potential recipient devices is less than a predetermined threshold; causing the UAV to navigate to the optimal intermediate location; sending, to each potential recipient device having a probability of requesting the payload carried by the UAV which exceeds a predetermined threshold, a notification indicating the payload carried by the unmanned aerial vehicle; receiving, from a first potential recipient device of the potential recipient devices, a request to deliver the payload; and causing the UAV to navigate from the optimal intermediate location to a location of the first potential recipient device when the request to deliver the payload is received.
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公开(公告)号:US11687869B2
公开(公告)日:2023-06-27
申请号:US16029076
申请日:2018-07-06
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
IPC: G05D1/02 , G06Q10/0833 , G06V20/13
CPC classification number: G06Q10/0833 , G05D1/0221 , G05D1/0246 , G05D1/0278 , G06V20/13 , G05D2201/0213
Abstract: A system and method for securing delivery of an autonomous vehicle. The method includes determining visual features of a captured image of a current location of the autonomous vehicle, the captured image generated by an image sensor communicatively coupled with the autonomous vehicle; retrieving location coordinates of the current location of the autonomous vehicle from a positioning sensor communicatively coupled with the autonomous vehicle; matching the visual features of the captured image to reference data associated with the location coordinates; and determining if the current location is the final destination. In some embodiments, the method further includes matching a verification code present within the captured image to a reference verification code, where the verification code is a two-dimensional visual code previously associated with the final destination.
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公开(公告)号:US12298762B2
公开(公告)日:2025-05-13
申请号:US18651168
申请日:2024-04-30
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
IPC: G05D1/00 , B64C39/02 , G05D1/689 , G05D1/692 , G08G5/00 , B64U10/14 , B64U101/60 , G05D1/81 , G06Q10/0832
Abstract: A system and method for aerial traffic management of unmanned aerial vehicles (UAVs) are provided. The method includes receiving at least a navigation request from a first UAV of a plurality of UAVs, wherein the navigation request specifies at least a waypoint; determining whether the waypoint is clear; sending an instruction the first UAV to hover at a specified position until the waypoint is clear, when the received waypoint is not clear; locking the waypoint, when the received waypoint not clear; and instructing the first UAV to navigate to the received waypoint.
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公开(公告)号:US12298761B2
公开(公告)日:2025-05-13
申请号:US18649542
申请日:2024-04-29
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
IPC: G05D1/00 , B64C39/02 , G05D1/689 , G05D1/692 , G08G5/00 , B64U10/14 , B64U60/50 , B64U70/83 , B64U101/60 , G05D1/81 , G06Q10/0832
Abstract: A system and method for safely terminating navigation of an unmanned aerial vehicle (UAV). A method includes generating a navigation plan for the UAV, the UAV including a propulsion system, wherein the navigation plan includes at least a start point, an end point, and a virtual three-dimensional (3D) tunnel connecting the start and end points; and configuring the UAV to execute the navigation plan by navigating from the start point to the end point, wherein the UAV is configured such that the UAV executes the navigation plan by navigating from the start point to the end point, wherein the UAV is further configured such that the UAV terminates navigation by terminating power to the propulsion system of the UAV and deploying a failsafe, wherein the UAV is configured to terminate navigation when the UAV is outside of the 3D tunnel.
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公开(公告)号:US10719086B2
公开(公告)日:2020-07-21
申请号:US15649133
申请日:2017-07-13
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
IPC: G01C22/00 , G05D1/00 , G05D1/10 , G05D1/02 , G08G5/00 , H04L29/08 , G05D3/00 , G06F7/00 , G06F17/00 , G01C23/00 , B64C39/02
Abstract: A system and method for dynamically updated vehicle navigation planning for a second UV based on navigation feedback of a first UV. The first UV navigates based on a first navigation plan and the second UV navigates based on a second navigation plan. The system includes: a processing circuitry; and a memory, the memory containing instructions that, when executed by the processing circuitry, configure the system to: receive the navigation feedback of the first UV, wherein the navigation feedback of the first UV includes telemetry data indicating at least a divergence event and a location of the divergence event, wherein the divergence event is a divergence of the first UV from the first navigation plan; and dynamically update the second navigation plan based on the navigation feedback of the first UV when the second navigation plan includes the location of the divergence event.
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公开(公告)号:US11762384B2
公开(公告)日:2023-09-19
申请号:US17014316
申请日:2020-09-08
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
IPC: G05D1/00 , B64C39/02 , G08G5/00 , G06Q10/0832 , B64U101/60
CPC classification number: G05D1/0027 , B64C39/024 , G05D1/0094 , G08G5/0013 , G08G5/0034 , G08G5/0043 , G08G5/0069 , G08G5/0082 , B64U2101/60 , B64U2201/20 , G05D1/0061 , G06Q10/0832
Abstract: A system and method for safely terminating navigation of an unmanned aerial vehicle (UAV). A method includes generating a navigation plan for the UAV, the UAV including a propulsion system, wherein the navigation plan includes at least a start point, an end point, and a virtual three-dimensional (3D) tunnel connecting the start and end points; and configuring the UAV to execute the navigation plan by navigating from the start point to the end point, wherein the UAV is configured such that the UAV executes the navigation plan by navigating from the start point to the end point, wherein the UAV is further configured such that the UAV terminates navigation by terminating power to the propulsion system of the UAV and deploying a failsafe, wherein the UAV is configured to terminate navigation when the UAV is outside of the 3D tunnel.
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公开(公告)号:US11720096B2
公开(公告)日:2023-08-08
申请号:US17014316
申请日:2020-09-08
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
IPC: G05D1/00 , B64C39/02 , G08G5/00 , G06Q10/0832 , B64U101/60
CPC classification number: G05D1/0027 , B64C39/024 , G05D1/0094 , G08G5/0013 , G08G5/0034 , G08G5/0043 , G08G5/0069 , G08G5/0082 , B64U2101/60 , B64U2201/20 , G05D1/0061 , G06Q10/0832
Abstract: A system and method for safely terminating navigation of an unmanned aerial vehicle (UAV). A method includes generating a navigation plan for the UAV, the UAV including a propulsion system, wherein the navigation plan includes at least a start point, an end point, and a virtual three-dimensional (3D) tunnel connecting the start and end points; and configuring the UAV to execute the navigation plan by navigating from the start point to the end point, wherein the UAV is configured such that the UAV executes the navigation plan by navigating from the start point to the end point, wherein the UAV is further configured such that the UAV terminates navigation by terminating power to the propulsion system of the UAV and deploying a failsafe, wherein the UAV is configured to terminate navigation when the UAV is outside of the 3D tunnel.
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公开(公告)号:US10274949B2
公开(公告)日:2019-04-30
申请号:US15447452
申请日:2017-03-02
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
Abstract: An apparatus and method for semi-automated control of a vehicle. The apparatus includes: a processing circuitry; and a memory, the memory containing instructions that, when executed by the processing circuitry, configure the apparatus to: establish control of the vehicle, wherein establishing the control further comprises determining a set of instructions for controlling the vehicle, wherein the apparatus is configured to control the vehicle based on the set of instructions during a first mode of control; receive at least one control instruction from a node, wherein the apparatus is configured to control, in real-time, the vehicle based on the set of instructions and the at least one control instruction received from the node during a second mode of control; determine, based on a predetermined list of mode changing events, a mode changing event; and change from the first mode to the second mode, when the mode changing event is determined.
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10.
公开(公告)号:US12159541B2
公开(公告)日:2024-12-03
申请号:US16429452
申请日:2019-06-03
Applicant: Flytrex Aviation Ltd.
Inventor: Yariv Bash , Amit Regev
IPC: G08G5/00
Abstract: A system and method for deploying multiple unmanned aerial vehicles (UAVs) from a single landing site. The method includes: generating a hovering perimeter for a landing site, the hovering perimeter including a plurality of hovering points and a plurality of approach vectors, each hovering point having spatial coordinates and being uniquely associated with one of the plurality of approach vectors, wherein a flight path based on a first approach vector of the plurality of approach vectors does not overlap with a flight path based on a second approach vector of the plurality of approach vectors; and configuring a first UAV of a plurality of UAVs to: navigate to a first hovering point of the plurality of hovering points; hover at the first hovering point; and navigate from the first hovering point to the landing site when the first UAV is authorized to land at the landing site.
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