Gulfstream Aerospace Corporation

Securaplane Technologies, Inc.

Jason Meade

Robert O'Dell

Frank Manochio

Michael Boost

Jamie Clive Marshall

Jeffrey Hausmann

Jimmy Lee Hancock, Jr

Gary M Freeman

Robert Odell

The disclosed embodiments relate to methods and systems for avoiding a collision between an aircraft on the ground and an obstacle using a three-dimensional visual indication of the area or plane of winglets on the wingtips of the aircraft. The method includes receiving a video image from a camera positioned in one of the winglets, the video image representing a field of view through which the winglet of the aircraft will pass along a present heading of the aircraft. Next a processor determines a three-dimensional area or plane within the field of view through which the winglet of the aircraft will pass. An overlay is displayed within the field of view to assist the pilot in avoiding collisions with obstacles.

Methods and systems for avoiding a collision between an aircraft and an obstacle using a three-dimensional visual indication of an aircraft wingtip path

The disclosed embodiments relate to methods and systems for avoiding a collision between an aircraft on the ground and an obstacle using a three-dimensional visual indication of the area or plane of winglets on the wingtips of the aircraft. The method includes receiving a video image from a camera positioned in one of the winglets, the video image representing a field of view through which the winglet of the aircraft will pass along a present heading of the aircraft. Next a processor determines a three-dimensional area or plane within the field of view through which the winglet of the aircraft will pass. An overlay is displayed within the field of view to assist the pilot in avoiding collisions with obstacles within the field of view.

Methods and systems for avoiding a collision between an aircraft and an obstacle using a three dimensional visual indication of an aircraft wingtip path

A system for providing visual feedback in an aircraft having an actuatable component includes a controller providing automatic control of the actuatable component in an automatic mode and permitting manual control of the actuatable component in a manual mode. A handle assembly is in communication with the actuatable component to provide manual control of the actuatable component in the manual mode. The system also includes a light panel integrated with the handle assembly, in communication with said controller, and configured to selectively illuminate to inform a user of the mode of the actuatable component.

Systems and methods for providing visual feedback in aircraft

A system is provided that includes a detachable mounting apparatus. The detachable mounting apparatus is configured to be secured on an aircraft. The detachable mounting apparatus includes a detection system and a warning system. The detection system can detect objects in proximity to the aircraft and generate a detection signal when an object is detected in proximity to the aircraft. The warning system can generate at least one alarm signal that is perceptible outside the aircraft.

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Savannah, GA, United States of America

Jason Meade