Honeywell International Inc.

Nathan Krishnamoorthy

Sunitha Panchangam

Anoop S

Lawrence Surace

Justin Schassler

Anoop Surendran

Ankur Mathur

Vatsalya Surana

Methods and systems for providing reduced flaps takeoff or landing advice in an aircraft. The methods and systems include a display device and a processor in operable communication with the display device. The processor is configured to execute program instructions. The program instructions are configured to cause the processor to receive takeoff or landing performance data including weather data and runway conditions data for a plurality of runways at a destination aerodrome, calculate values of takeoff or landing performance parameters for a plurality of flap configurations for each of the plurality of runways, and present, on the display device, at least one of the values of takeoff or landing performance parameters.

Systems and methods for providing reduced flaps takeoff and landing advice

In some examples, a collision awareness system includes two cameras mounted on portions of a vehicle and processing circuitry configured to determine a position of an object based on an image captured by a first camera when the object is within a field of view of the first camera. The processing circuitry is further configured to determine the position of the object based on an image captured by a second camera when the object is within a field of view of the second camera. The processing circuitry is also configured to determine whether a distance between a future position of the vehicle and a current or future position of the object is less than a threshold level. In response to determine that the distance is less than the threshold level, the processing circuitry can generate an alert.

Collision awareness using cameras mounted on a vehicle

Systems and methods and disclosed for alerting improper inhibition of alerts of aircraft warning systems. In some examples, a method may include: determining whether an inhibition of a safety alert of a warning system of an aircraft is activated; upon determining that the inhibition is activated, determining whether the inhibition is improper under current or upcoming operating conditions of the aircraft, the current or upcoming operating conditions including a current or projected position of the aircraft and a weather condition at the current or projected position; and upon determining that the inhibition is improper under the current or upcoming operating conditions, alerting an operator of the aircraft to deactivate the inhibition.

Systems and methods for alerting improper inhibition of warning systems

Growing community of inventors

Bengaluru, India

Nathan Krishnamoorthy