公开(公告)号：US11928505B2

公开(公告)日：2024-03-12

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 ,  B64D43/00 ,  B64D45/04 ,  G06F3/14 ,  G06F9/48 ,  G06F18/2113 ,  G06F18/24 ,  G06T11/00 ,  G06V10/40 ,  G06V20/13

CPC classification number: G06F9/50 ,  B64D43/00 ,  B64D45/04 ,  G06F3/14 ,  G06F9/4881 ,  G06F18/2113 ,  G06F18/24 ,  G06T11/001 ,  G06V10/40 ,  G06V20/13 ,  G06F2209/509

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.

公开(公告)号：US20230127623A1

公开(公告)日：2023-04-27

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

IPC: B64C13/50 ,  B64C13/04 ,  B64C13/34 ,  F16D28/00 ,  F16D48/06 ,  F16D27/00

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.

公开(公告)号：US11484737B2

公开(公告)日：2022-11-01

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

IPC: A62C3/02 ,  B64D1/16 ,  G05D1/10 ,  B64C27/12 ,  G08G5/00 ,  B64D1/22 ,  G06V20/10

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.

公开(公告)号：US20210086911A1

公开(公告)日：2021-03-25

申请号：US16575497

申请日：2019-09-19

Applicant: LOCKHEED MARTIN CORPORATION

Inventor： Margaret M. Lampazzi ,  George Nicholas Loussides ,  Igor Cherepinsky

IPC: B64D45/00 ,  G05D1/00 ,  G08G5/00

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.

公开(公告)号：US20200090524A1

公开(公告)日：2020-03-19

申请号：US16134121

申请日：2018-09-18

Applicant: LOCKHEED MARTIN CORPORATION

Inventor： Igor Cherepinsky ,  Mark Daniel Ward ,  Paul Michael Shields ,  Margaret MacIsaac Lampazzi

IPC: G08G5/00 ,  G05D1/00 ,  G05D1/10 ,  G07C5/00

Abstract: According to an aspect, an apparatus is provided. A computing system is provided. A user interface is configured to receive an input from a user related to one or more changes to flight path and transmit the input to an autonomous flight system. The input to the autonomous flight system does not cause the autonomous flight system to disengage.