Honeywell International Inc.

Raghu Seelamonthula

Rajesh V Poojary

Manuj Sharma

Vinay Sridhara Murthy

Raghavendra Muniraju

Nipun Kumar Chawda

Sunil Venugopalan

Fazludeen Ruknudeen

Tracking aircraft in and near a ramp area is described herein. One system for tracking an aircraft, comprising: a sensor array, positioned at or near a ramp area at an airport, having a camera image sensor device and a light detection and ranging (LIDAR) sensor device that are both located at a single sensor array location with respect to the ramp area; the camera image sensor device configured to capture camera image data illustrating the aircraft while the aircraft is approaching or in the ramp area; the LIDAR sensor device configured to capture LIDAR sensor device data illustrating the aircraft while the aircraft is approaching or in the ramp area.

Multi-sensor data fusion-based aircraft detection, tracking, and docking

Tracking aircraft in and near a ramp area is described herein. One method includes receiving camera image data of an aircraft while the aircraft is approaching or in the ramp area, receiving LIDAR/Radar sensor data of an aircraft while the aircraft is approaching or in the ramp area, merging the camera image data and the LIDAR/Radar sensor data into a merged data set, and wherein the merged data set includes at least one of: data for determining the position and orientation of the aircraft relative to the position and orientation of the ramp area, data for determining speed of the aircraft, data for determining direction of the aircraft, data for determining proximity of the aircraft to a particular object within the ramp area, and data for forming a three dimensional virtual model of at least a portion of the aircraft from the merged data.

A constant current regulator for airfield ground lighting is described herein. For example, one or more embodiments include a power converter configured to receive a signal from an alternating current (AC) mains, where the power converter includes a number of bi-directional switches, a transformer configured to isolate the AC signal from an airfield ground lighting circuit, and a rectifier configured to convert the signal from the AC mains from AC to direct current (DC), an inverter configured to convert the DC signal from the power converter and convert the DC to AC, an output filter configured to receive the AC signal from the inverter and send the AC signal to the airfield ground lighting circuit, and a controller configured to switch the number of bi-directional switches of the power converter to allow an input voltage and current of the signal from the AC mains to be in phase.

Constant current regulator for airfield ground lighting

Methods and systems for updating an airfield lighting system with an LED light source are described herein. One method includes removing a light source from an existing light fixture of an airfield lighting system, wherein the removed light source is not a light emitting diode (LED) light source, and replacing the removed light source with an LED light source in the existing light fixture without modifying or replacing any other element of the existing light fixture.

Growing community of inventors

Bengaluru, India

Raghu Seelamonthula