Lockheed Martin Corporation

Sikorsky Aircraft Corporation

Michael Aaron Connor

Igor Cherepinsky

Harshad S Sane

Robert S Takacs

Christopher Stathis

George Nicholas Loussides

Margaret MacIsaac Lampazzi

Joshua M Leland

Carl John Pankok, Jr

Marc A Antonetz

Nicholas Visinski

Christopher J Marini

Grace Valeria Tilton

Ashley M Currivan

Jesse Elia Morzel

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.

Systems and methods for automation of cockpit switches

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.

Actuation system for cockpit control levers

A communication system includes a vehicle communication assembly connected to a vehicle, including a transmitter and a receiver, and configured to wirelessly communicate with a remote entity, and a processing device and a memory coupled to the processing device. The memory includes computer-executable instructions that, when executed by the processing device, cause the processing device to receive a wireless signal including a speech communication from the remote entity at the receiver, analyze the wireless signal by a speech recognition module to identify the speech communication, and recognize a known directive within the speech communication based on stored contextual information. The instructions also cause the processing device to, based on recognizing the known directive, present a textual representation of the known directive to a user of the vehicle, and determine that the processing device correctly recognized the known directive based on detecting an input from the user verifying the known directive.

Verification of wireless communications between a vehicle user and a remote entity

An aircraft and method of operating an aircraft. A sensor measures an air velocity at a location a selected distance from the aircraft. A processor determines an effect of the air velocity on an accuracy metric of a first flight course of the aircraft, changes from the first flight course to a second flight course when the accuracy metric of the first flight course meets a threshold and operates the aircraft according to the second flight course.

Optimal path planning with optical air velocity sensing

An apparatus for guiding an aircraft includes: an air velocity sensor disposed on the aircraft and configured to sense a speed and direction of a wind remote to the aircraft to provide remote wind speed and direction data; a flight control actuator coupled to a flight control device; and a flight controller communicably coupled to the air velocity sensor, the flight controller having an input section that receives the remote wind speed and direction data from the air velocity sensor, a processor configured to determine a magnitude and direction of the wind with respect to a planned flight route and to predict an influence acting on the aircraft due to the magnitude and direction of the wind with respect to the planned flight route, and an output section communicably coupled to the flight control actuator to provide a control signal that results in the aircraft counteracting the predicted influence.

Predictive wind gust alleviation using optical velocity sensing

According to an aspect, a releasable actuation system includes a support member, a carriage movable relative to the support member, a releasable mount configured to couple the support member to a frame, the support member being rotatable relative to the releasable mount by a rotatable joint, an image capturing sensor connected to the carriage, an actuator connected to the carriage and operable to adjust a position of a switch, a memory having computer readable instructions, and one or more processors for executing the computer readable instructions, the computer readable instructions controlling the one or more processors to perform operations comprising directing the actuator to adjust the position of the switch.

Automated switch activation system

An active sensing system includes an agent and at least one sensor operatively associated with the agent. The at least one sensor includes one or more emitters configured and disposed to establish a sensing zone. A conflict identification module is configured and disposed to identify one or more sensor conflict regions, and an active sensor controller is operatively connected to the at least one sensor and the conflict identification module. The active sensor controller is configured and disposed to form an adjustment zone within the sensing zone to accommodate the one or more sensor conflict regions.

Active sensing system and method of sensing with an active sensor system

A vehicle access and control system includes an activation system, a vehicle control system, a communication system provided in the vehicle, a computer system mounted in the vehicle, and a vehicle access control system including a processor, a non-volatile memory, and a set of instructions stored on the non-volatile memory. The set of instructions, when executed by the processor, causing the processor to receive a user specific identification input, access a user profile associated with the user specific identification input, determine, from the user profile, system permissions associated with the user specific identification input, and manage access to one or more of the activation system, vehicle control system, communication system, and the computer system based on the system permissions.

Vehicle access control system and method

A method of communication link accessibility aware navigation is provided that includes querying a communication link accessibility map based on a location of interest provided by a path planner for a communication node. A communication link accessibility indicator is received representing a communication link characteristic associated with the location of interest in response to querying the communication link accessibility map. A communication link accessibility weight is determined based on a mission priority of maintaining a communication link of the communication node. The communication link accessibility weight is applied to the communication link accessibility indicator.

Communication link accessibility aware navigation

A system and method for identifying a slung load for an aircraft with one or more sensors includes receiving, with a processor via one or more sensors, sensor information related to flight dynamics data for the aircraft; determining, with the processor, control input commands for the aircraft in response to the receiving of the flight dynamics data; determining, with the processor, signals indicative of an estimated pendulum frequency; and determining, with the processor, parameters associated with the slung load in response to the determining of the estimated pendulum frequencies.

Slung load identification with aircraft flight dynamics data

A method and system for sharing information between independent agents having a processor and memory having instructions stored thereon that, when executed by the processor, cause the system to receive signals indicative of a fault of a sensor system of a first independent agent; transmit signals indicative of a request for sensor information to a second independent agent; receive signals indicative of state information for the second independent agent in response to the receiving of the request for sensor information; and apply the state information to a navigation system of the first independent agent in response to the receiving of the state information.

Growing community of inventors

New Haven, CT, United States of America

Michael Aaron Connor