Honeywell International Inc.

Intel Corporation

Intel Corproation

Andrew Fannon Lamkin

Duke Buster

Jeffrey W Starr

Matthew Warpinski

Hong W Wong

Bradford H Needham

Joseph J Nutaro

Jiri Vasek

James Christopher Kirk

Matej Dusik

Phillip J Kearns

Christopher Montano

PerriLynne Silva

Joseph Duval

Katherine P Anthony

Perrilynne Silva

Apparatus, method and storage medium associated with UAV assisted emergency responses are disclosed herein. In embodiments, an UAV may comprise a flight controller to control at least one or more engines of the UAV to navigate the UAV to condition road traffic for an emergency vehicle on emergency en route to a destination, wherein to condition road traffic, the flight controller is to receive navigation data of the emergency vehicle, and in response, control at least the one or more engines to navigate the UAV in advance of the emergency vehicle, to alert road traffics ahead of the emergency vehicle of pending transit of the emergency vehicle. Other embodiments may be disclosed or claimed.

Emergency UAV method and apparatus

Embodiments of a system and method for method for automatically determining pet owner interaction with a pet are generally described herein. A method may include obtaining sensor data including pet behavior metrics from a sensor, aggregating the sensor data, and interpreting the aggregated sensor data to determine an engagement factor of a pet owner to a pet. The method may include outputting a report based on the engagement factor or the aggregated sensor data.

Pet owner evaluation system

Embodiments of the subject matter described herein provide an innovative method and system capable of enabling external ground control of a manned aircraft without a pilot or crew, in order to (i) move the aircraft, and (ii) command various subsystems of the aircraft. The provided method and system supports secure wireless communication between the aircraft and a remote device.

External aircraft ground control

Systems and methods for location aware augmented vision aircraft monitoring and inspection are provided. In one embodiment, a method for location aware augmented vision assisted aircraft inspection and monitoring comprises: obtaining status information regarding an aircraft from an on-board aircraft network; obtaining a user location from a user carried augmented vision display device; refining a first data set from the status information based at least in part on the user location; wirelessly transmitting the first data set to the user carried augmented vision display device; determining an orientation of the user carried augmented vision display device with respect to the aircraft; and displaying at least a subset of the first data set on the user carried augmented vision display device, wherein the subset of the first data set is determined at least in part based on the orientation of the user carried augmented vision display device.

Systems and methods for location aware augmented vision aircraft monitoring and inspection

Various techniques for performing camera control techniques based on brainwave data from an electroencephalography (EEG) headset are disclosed herein. In an example, a computing system operates to receive brainwave data representing brainwave activity, process the brainwave data, and transmit a command to a camera device based on the processed brainwave data. For example, the brainwave data may correlate to raw brainwave signals (from gamma, beta, alpha, theta, or delta brainwaves), or composite brainwave signals (from multiple brainwaves, representative of attention, meditation, or like states). As a result, the computing system may transmit a command to a camera device to capture an image, a burst of images, start/stop video recording, or like commands for image and video operations, based on a human user's detected brainwave state. Further processing, detection, and training methods for brainwave control of camera operations are also disclosed.

Electroencephalography (EEG) camera control

A ground obstacle collision-avoidance system includes a plurality of radar sensor modules that each receive at a radar detector radar return signals corresponding to reflections of the emitted signal from a ground obstacle, and transmits radar information associated with the received radar signal reflections reflected from the ground obstacle, wherein each of the plurality of radar sensor modules are uniquely located on a surface of an aircraft that is at risk for collision with a ground obstacle if the aircraft is moving; a gateway unit that receives the radar information transmitted from the radar sensor module and transmits information associated with the received radar information; a processing system configured to determine a distance from the installation aircraft to a detected ground object detected; and a display configured to present a plan view indicating an aircraft icon and a graphical ground obstacle icon that is associated with the detected ground obstacle.

Collision-avoidance system for ground crew using sensors

In some examples, a brake wear measurement system includes an emitter configured to emit a signal and a passive powered sensor system including a controller and a sensor configured to sense the signal emitted by the emitter. The emitter and the sensor of the sensor system are mounted on the brake assembly such as the emitter and the sensor may be configured to move relative to each other as the brake disc stack wears. Thus, a characteristic of the signal emitted by the emitter and sensed by the sensor may change as a function of the brake disc stack wear. The brake wear measurement may further include a processor configured to receive the output generated by the sensor and determine, based on the output, an amount of wear of the brake disc stack assembly.

Brake disc stack wear measurement

In sonic examples, an obstacle detection system is configured to generate and display a graphical user interface (GUI) that includes an overhead image of an area in which a vehicle is positioned, a graphical representation of the vehicle, and graphical representations of one or more obstacles, The graphical representations of the one or more obstacles and vehicle can be arranged relative to the overhead image to indicate determined real-world positions of the one or more obstacles and vehicle, respectively, relative to other features shown in the overhead (e.g., airport structure or other buildings).

Obstacle detection system providing context awareness

An environmental impact measurement system for an aircraft includes a one-way data interface and a processing system. The one-way data interface is adapted to continuously receive and transmit aircraft data and flight plan data. The processing system is in operable communication with the one-way data interface to receive the aircraft data and the flight plan data transmitted therefrom. The processing system is configured, upon receipt of the aircraft data and the flight plan data, to generate at least data representative of real-time environmental impact of the aircraft, and recommendations for improving the real-time environmental impact of the aircraft.

Aircraft environmental impact measurement system

A ground crew collision-avoidance system includes a plurality of radar sensor modules that each emit a radar signal, receives at a radar detector radar return signals corresponding to reflections of the emitted signal from a ground object, and transmits radar information associated with the received radar signal reflections reflected from the ground object, wherein each of the plurality of radar sensor modules are uniquely located on a surface of an aircraft that is at risk for collision with a ground object while the aircraft is being towed; a gateway unit that receives the radar information transmitted from the radar sensor module and transmits information associated with the received radar information; and a ground crew alert indicator that receives the information transmitted by the gateway unit and that presents a graphical alert icon on a display. The display indicates a likelihood of collision between the aircraft and the ground object.

Systems and methods for performing airport surface collision-avoidance. A wingtip-mounted camera allows the pilot to positively ascertain that the wingtip will clear objects located in the video. An exemplary system implemented on an aircraft includes a wingtip module having a camera that generates a video stream and a communication device that transmits the generated video stream. A processor receives the video stream and generates a reticule for the video stream. A display device simultaneously presents the video stream and the reticule. The reticule includes a horizon line and is based on a focal length of a lens of the camera and height of the camera above ground. The reticule includes curved and/or straight distance lines and curved or straight travel lines. The travel line(s) correspond to at least one aircraft component or a zone of importance and are based on location of the camera and trajectory of the aircraft.

Growing community of inventors

Albuquerque, NM, United States of America

Andrew Fannon Lamkin