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公开(公告)号：US11787527B2
公开(公告)日：2023-10-17
申请号：US17511349
申请日：2021-10-26
Applicant: Lockheed Martin Corporation
Inventor： Michael A Connor , Igor Cherepinsky , Christopher J. Marini , Nicholas Visinski , Ashley M. Currivan
CPC classification number: B64C13/50 , B64C13/0421 , B64C13/34 , F16D27/00 , F16D28/00 , F16D48/06 , F16D2500/1023
Abstract: An actuation system for an aircraft can include an actuator and a plurality of clutches connected to and structured to be moved by the actuator. The actuation system can include a plurality of control levers connected to the plurality of clutches and structured to be moved by the plurality of clutches when the plurality of clutches are moved by the actuator. The actuation system can include a processor connected to the actuator and to the plurality of clutches. The processor can identify one or more clutches connected to one or more control levers of the plurality of control levers for controlling an operation of the aircraft, and cause the one or more clutches connected to the one or more control levers to be in an engaged stat. The processor can activate the actuator to cause movement of the one or more control levers via the one or more clutches.
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公开(公告)号：US20230227173A1
公开(公告)日：2023-07-20
申请号：US17577878
申请日：2022-01-18
Applicant: Lockheed Martin Corporation
Inventor： Michael A. Connor , Jesse Elia Morzel , Marc A. Antonetz , Igor Cherepinsky
CPC classification number: B64D43/00 , H01H47/226
Abstract: A cockpit switch device can include a pushbutton switch, a bi-stable relay and a toggle component. The pushbutton switch can be configured to be manually actuated by a user into a command state. The bi-stable relay can be controlled by input commands from the pushbutton switch and input commands from a processor, and can be configured to control operation of one or more systems of an a aircraft. The toggle component can be connected to the pushbutton switch, the processor and the bi-stable relay. The toggle component can receive an input command signal from at least one of the pushbutton switch or the processor, and cause a state of the bi-stable relay to be flipped responsive to the input command signal from the at least one of the pushbutton switch or the processor.
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公开(公告)号：US11592843B2
公开(公告)日：2023-02-28
申请号：US16843011
申请日：2020-04-08
Applicant: Lockheed Martin Corporation
Inventor： Navid Dadkhah Tehrani , Brian Henri Le Floch , Ashish Bhatnagar , Suraj Unnikrishnan , Brian Scott MacAllister , Igor Cherepinsky
Abstract: A technique relates to autonomous obstacle avoidance. A vehicle is controlled on a route to a destination, the route being a three-dimensional route. An obstruction is determined on the global route. A local route including alternate points to avoid the obstruction is autonomously determined. The local route is autonomously converged back to the global route in response to avoiding the obstruction.
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公开(公告)号：US20210370110A1
公开(公告)日：2021-12-02
申请号：US16886828
申请日：2020-05-29
Applicant: LOCKHEED MARTIN CORPORATION
Inventor： Carl John Pankok, Jr. , Michael Paul Baran , Sean Scott Carlson , George Nicholas Loussides , Alexander Quinn Weintraub , Igor Cherepinsky
Abstract: According to an aspect, a computer-implemented method for water volume estimation includes detecting water based at least in part on sensor-based data; determining a volume of water based at least in part on the sensor-based data; determining a location at the water for an aircraft to retrieve water via a water retrieving apparatus; and translating the location of the water into pilot inputs to guide the aircraft to the water.
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公开(公告)号：US20210318697A1
公开(公告)日：2021-10-14
申请号：US16843011
申请日：2020-04-08
Applicant: Lockheed Martin Corporation
Inventor： Navid Dadkhah Tehrani , Brian Henri Le Floch , Ashish Bhatnagar , Suraj Unnikrishnan , Brian Scott MacAllister , Igor Cherepinsky
Abstract: A technique relates to autonomous obstacle avoidance. A vehicle is controlled on a route to a destination, the route being a three-dimensional route. An obstruction is determined on the global route. A local route including alternate points to avoid the obstruction is autonomously determined. The local route is autonomously converged back to the global route in response to avoiding the obstruction.
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Patent Agency Ranking
公开(公告)号：US20220009651A1
公开(公告)日：2022-01-13
申请号：US16923143
申请日：2020-07-08
Applicant: Lockheed Martin Corporation
Inventor： Margaret MacIsaac Lampazzi , Carl John Pankok, JR. , Igor Cherepinsky
IPC: B64F5/60 , G06F3/0482
Abstract: A technique relates to interactive aircraft operation. An interactive electronic checklist is selected from a plurality of interactive electronic checklists, the interactive electronic checklists each comprising checklist tasks. It is perceived that one or more of the checklist tasks in the interactive electronic checklist is executable by an autonomous system. The one or more of the checklist tasks is performed using the autonomous system, an operator being designated to perform any other ones of the checklist tasks.
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公开(公告)号：US12060158B2
公开(公告)日：2024-08-13
申请号：US17577878
申请日：2022-01-18
Applicant: Lockheed Martin Corporation
Inventor： Michael A. Connor , Jesse Elia Morzel , Marc A. Antonetz , Igor Cherepinsky
CPC classification number: B64D43/00 , H01H47/226
Abstract: A cockpit switch device can include a pushbutton switch, a bi-stable relay and a toggle component. The pushbutton switch can be configured to be manually actuated by a user into a command state. The bi-stable relay can be controlled by input commands from the pushbutton switch and input commands from a processor, and can be configured to control operation of one or more systems of an aircraft. The toggle component can be connected to the pushbutton switch, the processor and the bi-stable relay. The toggle component can receive an input command signal from at least one of the pushbutton switch or the processor, and cause a state of the bi-stable relay to be flipped responsive to the input command signal from the at least one of the pushbutton switch or the processor.
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公开(公告)号：US11447272B2
公开(公告)日：2022-09-20
申请号：US16923143
申请日：2020-07-08
Applicant: Lockheed Martin Corporation
Inventor： Margaret MacIsaac Lampazzi , Carl John Pankok, Jr. , Igor Cherepinsky
IPC: B64F5/60 , G06F3/0482
Abstract: A technique relates to interactive aircraft operation. An interactive electronic checklist is selected from a plurality of interactive electronic checklists, the interactive electronic checklists each comprising checklist tasks. It is perceived that one or more of the checklist tasks in the interactive electronic checklist is executable by an autonomous system. The one or more of the checklist tasks is performed using the autonomous system, an operator being designated to perform any other ones of the checklist tasks.
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公开(公告)号：US20220365816A1
公开(公告)日：2022-11-17
申请号：US17318815
申请日：2021-05-12
Applicant: LOCKHEED MARTIN CORPORATION
Inventor： Navid Dadkhah Tehrani , Daniel Montrallo Flickinger , Igor Cherepinsky
IPC: G06F9/50 , G06F9/48 , B64D43/00 , B64D45/04 , G06F3/14 , G06K9/62 , G06K9/46 , G06K9/00 , G06T11/00
Abstract: Offline task-based feature processing for aerial vehicles is provided. A system can extract features from a world model generated using sensor information captured by sensors mounted on an aerial vehicle. The system generates a label for each of the features and identifies identify processing levels based on the features. The system selects a processing level for each feature of a subset of features based on a task performed by the aerial vehicle and the label associated with the feature. The system generates one or more processed features by applying the processing level to a respective feature of the subset of the plurality of features. The system presents the one or more processed features on a display device of the aerial vehicle.
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公开(公告)号：US11186384B2
公开(公告)日：2021-11-30
申请号：US16575497
申请日：2019-09-19
Applicant: LOCKHEED MARTIN CORPORATION
Inventor： Margaret M. Lampazzi , George Nicholas Loussides , Igor Cherepinsky
Abstract: A technique relates to adaptive flight display. The technique includes rendering a first flight instrument display during autonomous flight operation of an aircraft, the first flight instrument display comprising autonomous mode information; determining, by a processor, that a trigger is met to transition from the first flight instrument display for the autonomous flight operation to a second flight instrument display for providing an increased perception of aircraft operating parameters for at least one of increased human awareness and human operation of the aircraft, the trigger being associated with a requirement for human intervention; and in response to the trigger being met, rendering the second flight instrument display for the human operation of the aircraft, the second flight instrument display comprising additional information.
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