Honeywell International Inc.

Duke Buster

Andrew Fannon Lamkin

Jeffrey W Starr

Matthew Warpinski

Joseph J Nutaro

Randolph G Hartman

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

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 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.

A method for marking a position of a real world object on a see-through display is provided. The method includes capturing an image of a real world object with an imaging device. A viewing angle and a distance to the object are determined. A real world position of the object is calculated based on the viewing angle to the object and the distance to the object. A location on the see-through display that corresponds to the real world position of the object is determined. A mark is then displayed on the see-through display at the location that corresponds to the real world object.

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Albuquerque, NM, United States of America

Duke Buster